View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 68954U 26145.58335647 +.00000000 +00000-0 +43368-3 0 00001
2 68954 53.1594 268.7016 0001116 46.3712 105.9306 15.49280466 02
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001116 |
| inclination: | 53.1594° |
| perigee height: | 418 km |
| apogee height: | 420 km |
| right ascension of ascending node: | 268.7016° |
| argument of perigee: | 46.3712° |
| revolutions per day: | 15.49280466 |
| mean anomaly at epoch: | 105.9306° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|