View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 68730U 26145.58335647 +.00000000 +00000-0 -41720-1 0 00002
2 68730 97.2846 9.3745 0001774 103.5054 189.5277 15.55398550 02
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001774 |
| inclination: | 97.2846° |
| perigee height: | 400 km |
| apogee height: | 402 km |
| right ascension of ascending node: | 9.3745° |
| argument of perigee: | 103.5054° |
| revolutions per day: | 15.55398550 |
| mean anomaly at epoch: | 189.5277° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|