View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 08799U 26088.08202863 +.00000000 +00000-0 +35705-4 0 00003
2 08799 81.2541 306.3902 0035224 82.2512 278.2657 14.11891997 02
| Epoch (UTC): | 29 March 2026 01:58:07 |
| Eccentricity: | 0.0035224 |
| inclination: | 81.2541° |
| perigee height: | 827 km |
| apogee height: | 878 km |
| right ascension of ascending node: | 306.3902° |
| argument of perigee: | 82.2512° |
| revolutions per day: | 14.11891997 |
| mean anomaly at epoch: | 278.2657° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|