View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 58929U 26145.64238102 +.00000000 +00000-0 +58763-3 0 00002
2 58929 96.6210 30.6954 0003002 80.2211 279.9395 15.75397500 01
| Epoch (UTC): | 25 May 2026 15:25:01 |
| Eccentricity: | 0.0003002 |
| inclination: | 96.6210° |
| perigee height: | 341 km |
| apogee height: | 346 km |
| right ascension of ascending node: | 30.6954° |
| argument of perigee: | 80.2211° |
| revolutions per day: | 15.75397500 |
| mean anomaly at epoch: | 279.9395° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|