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 24278.72390829 .00000420 00000-0 21989-3 0 9995
2 08800 81.2499 142.7745 0093832 193.7882 166.0726 14.10469433493801
| Epoch (UTC): | 04 October 2024 17:22:25 |
| Eccentricity: | 0.0093832 |
| inclination: | 81.2499° |
| perigee height: | 790 km |
| apogee height: | 925 km |
| right ascension of ascending node: | 142.7745° |
| argument of perigee: | 193.7882° |
| revolutions per day: | 14.10469433 |
| mean anomaly at epoch: | 166.0726° |
| orbit number at epoch: | 49380 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|