Where could I get real time telemetries for OSIRIS-REX?
For deep space missions, the spacecraft don't really "know" where they are and don't send position information back to Earth in telemetry as such.
Instead, people here interpret signals from the spacecraft (mostly round-trip time delays and doppler shifts) to get line-of-sight distance and speed. Over time this is compiled, and matched with a numerical orbit simulator based on gravity from all solar system objects, radiation pressure from the Sun, and other effects.
I believe the best that you can do is to look at the predicted future orbit in JPL's Horizons ephemeris. Right now the trajectory there is dated March 27, 2018, and the evens and maneuvers are specified to much finer detail than "midnight".
This will not reflect exactly where the spacecraft is, but it is likely that if the mission has deviated substantially from this plan, an updated ephemeris will be posted sooner or later.
For detailed directions with screenshots for how to download a table of positions and velocities (together known as state vectors) from Horizons, see this answer.
You may also want to review this answer to the question How to show spacecraft position, heading etc relative to an asteroid? which discusses relative vectors between OSIRIS-REx and the asteroid Bennu.
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Currently the HORIZONS header for OSIRIS-REx state vectors includes:
Revised: Mar 27, 2018 OSIRIS-REx Spacecraft / (Sun) -64
http://www.asteroidmission.org
https://directory.eoportal.org/web/eoportal/satellite-missions/o/osiris-rex
http://www.nasa.gov/sites/default/files/atoms/files/osiris-rex_press_kit_0.pdf
NOTE:
2017-Sep-22 Earth gravity-assist flyby:
Closest-approach is nominally at 16:51:46 UTC, 23592 km from Earth center,
over 271.89346 deg. E, -74.80121 deg. (South). This is over Antarctica,
south of the tip of South America, about 420 km north of Vinson Massif,
the highest point in Antarctica.
BACKGROUND
OSIRIS-REx will explore 101955 Bennu (1999 RQ36), a carbonaceous B-type
asteroid whose regolith may provide insights on the early history of the
solar system.
MISSION EVENT SUMMARY (UTC)
2016 Sep 08 23:05 Launch from Cape Canaveral; daily 120 minutes windows from
Sep 8 - Oct 12. Atlas V w/Centaur upper stage.
2017 Sep 22 16:52 Earth flyby and gravity assist 23,592 km from geocenter
over {-74.80121 deg. S, 271.89346 deg. E}
2018 Aug Bennu approach phase
Oct Rendevous with asteroid
Nov Estimate mass, shape, and spin state models
2019 Jan Begin detailed mapping; identify candidate sample sites
May Sorties to examine 4 candidate sample sistes
Sep Collect sample > 60 grams
Oct Quiescent operations in Bennu's heliocentric orbit
2021 Mar Start return cruise and transport sample back to Earth
2023 Sep 24 Sample recovery on Earth
MISSION OBJECTIVES
* Map the asteroid
* Return and analyze a sample of Bennu's surface
* Document the sample site
* Measure the orbit deviation caused by small non-gravitational forces
* Compare observations made at the asteroid to ground-based observations
SPACECRAFT PHYSICAL DATA:
Length : 20.25 ft (6.2 m) with solar panels deployed
Width : 8 ft (2.4 m) x 8 ft (2.4 m)
Height : 10.33 ft (3.2 m)
TAGSAM Length : 11 ft (3.4 m) ("Touch-and-Go Camera System")
Dry mass (unfueled): 1,940 lbs (880 kg)
Wet mass (fueled) : 4,650 lbs (2,110 kg)
Power : Two solar panels 91 ft^2 (8.5 m^2) generate 1226 to
3000 watts, depending on distance from the Sun
SPACECRAFT TRAJECTORY
Post-launch spacecraft reference trajectory. Updated as warranted, as the
mission progresses. Corresponding Bennu trajectory is JPL #76, sb-101955-76.
[NOTE: To generate ephemerides of the destination asteroid (Bennu) (i.e.,
as a target), do a look-up using integer code "2101955" (NO semi-colon).
To use the asteroid as an observing point (i.e., produce ephemerides
relative to Bennu), set the coordinate center to "@2101955".]
Trajectory name Start (TDB) Stop (TDB)
------------------------------------ ----------------- -----------------
orx_160909_171201_170830_od023_v1 2016-Sep-09 07:00 2017-May-01 00:01
orx_170501_180710_171005_od027_v1 2017-May-01 00:00 2017-Oct-06 00:01
orx_171006_231024_171005_refod027_v1 2017-Oct-06 00:01 2023-Oct-23 00:00