View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 54214U 26145.58147751 +.00000000 +00000-0 +59543-4 0 00005
2 54214 59.9978 15.0599 0008442 299.4753 60.5440 14.29512984 05
| Epoch (UTC): | 25 May 2026 13:57:19 |
| Eccentricity: | 0.0008442 |
| inclination: | 59.9978° |
| perigee height: | 787 km |
| apogee height: | 799 km |
| right ascension of ascending node: | 15.0599° |
| argument of perigee: | 299.4753° |
| revolutions per day: | 14.29512984 |
| mean anomaly at epoch: | 60.5440° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|