View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 32156U 99025CTA 23263.51391192 .00001489 00000-0 58787-3 0 9999
2 32156 99.2764 5.0574 0085329 239.4723 119.8014 14.28736509843211
| Epoch (UTC): | 20 September 2023 12:20:01 |
| Eccentricity: | 0.0085329 |
| inclination: | 99.2764° |
| perigee height: | 735 km |
| apogee height: | 857 km |
| right ascension of ascending node: | 5.0574° |
| argument of perigee: | 239.4723° |
| revolutions per day: | 14.28736509 |
| mean anomaly at epoch: | 119.8014° |
| orbit number at epoch: | 84321 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|