View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 65796U 26145.39585100 +.00000000 +00000-0 +25516-3 0 00007
2 65796 97.4489 8.2067 0002503 85.5868 274.5645 15.05658689 05
| Epoch (UTC): | 25 May 2026 09:30:01 |
| Eccentricity: | 0.0002503 |
| inclination: | 97.4489° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 8.2067° |
| argument of perigee: | 85.5868° |
| revolutions per day: | 15.05658689 |
| mean anomaly at epoch: | 274.5645° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|