View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 08800U 76032B 23341.36953782 .00000279 00000-0 14464-3 0 9990
2 08800 81.2520 77.0696 0093576 331.9932 27.6219 14.10336344451186
| Epoch (UTC): | 07 December 2023 08:52:08 |
| Eccentricity: | 0.0093576 |
| inclination: | 81.2520° |
| perigee height: | 790 km |
| apogee height: | 926 km |
| right ascension of ascending node: | 77.0696° |
| argument of perigee: | 331.9932° |
| revolutions per day: | 14.10336344 |
| mean anomaly at epoch: | 27.6219° |
| orbit number at epoch: | 45118 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|