View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 54857U 26145.14014910 +.00000000 +00000-0 +10256-3 0 00007
2 54857 43.0054 49.7517 0001466 268.0008 92.0676 15.27578662 00
| Epoch (UTC): | 25 May 2026 03:21:48 |
| Eccentricity: | 0.0001466 |
| inclination: | 43.0054° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 49.7517° |
| argument of perigee: | 268.0008° |
| revolutions per day: | 15.27578662 |
| mean anomaly at epoch: | 92.0676° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|