- #1
Philosophaie
- 462
- 0
M(t) = M0 + n (t - t0)
where M(t) = the Mean Anomaly at time t;
M0 = the Mean Anomaly at the Epoch time;
n = (G*(Me+Msat)/a^2)^.5 = the satellite orbit's Mean Motion;
t = the chosen prediction time; and
t0 = the Epoch time.
My question is what are the time units in (Days, Hours, etc)?
where M(t) = the Mean Anomaly at time t;
M0 = the Mean Anomaly at the Epoch time;
n = (G*(Me+Msat)/a^2)^.5 = the satellite orbit's Mean Motion;
t = the chosen prediction time; and
t0 = the Epoch time.
My question is what are the time units in (Days, Hours, etc)?