View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 68992U 26145.47401309 +.00000000 +00000-0 +15081-3 0 00001
2 68992 97.7394 43.3426 0002502 192.9786 167.1368 14.91355792 06
| Epoch (UTC): | 25 May 2026 11:22:34 |
| Eccentricity: | 0.0002502 |
| inclination: | 97.7394° |
| perigee height: | 592 km |
| apogee height: | 595 km |
| right ascension of ascending node: | 43.3426° |
| argument of perigee: | 192.9786° |
| revolutions per day: | 14.91355792 |
| mean anomaly at epoch: | 167.1368° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|