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Tarlan Mammadzada's user avatar
Tarlan Mammadzada's user avatar
Tarlan Mammadzada's user avatar
Tarlan Mammadzada
  • Member for 7 years, 2 months
  • Last seen more than a month ago
  • Baku, Azerbaijan
9 votes
3 answers
2k views

Getting state vectors from JPL Horizons ephemerides

8 votes
1 answer
1k views

Multiple solutions to Lambert's problem

7 votes
3 answers
10k views

How to generate TLE file?

5 votes
2 answers
1k views

Sun-synchronous satellite orbit propagation

5 votes
5 answers
2k views

How to determine an algorithm for Low Earth Orbit propagation, considering perturbation from the moon, sun, etc?

4 votes
4 answers
8k views

SGP4 TEME frame to J2000 conversion

3 votes
3 answers
391 views

Interpolate the ephemerides of the Earth

3 votes
1 answer
598 views

Equation of motion for Geocentric orbit

3 votes
2 answers
3k views

Lambert's problem solution: optimal transfer time

2 votes
1 answer
283 views

The delta V required for given cordinates intersection on given time

2 votes
1 answer
175 views

Flying to orbital nodes

2 votes
1 answer
3k views

Cubesat 6U and 12U maximum weight

2 votes
1 answer
389 views

How can you calculate the minimal cone angle between two satellites to prevent interference?

2 votes
1 answer
1k views

SGP4: propagation initialization by state vector

1 vote
1 answer
288 views

Calculate the state vector of planets and moons

1 vote
1 answer
858 views

Inclination change maneuver [duplicate]

0 votes
1 answer
410 views

How long would a satellite fly on a sun-synchronous 600km orbit?

0 votes
1 answer
3k views

TLE data conversion to osculating orbit elements [closed]