View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 55924U 26145.24790366 +.00000000 +00000-0 -26824-4 0 00000
2 55924 69.9992 91.5961 0003218 268.6144 91.4646 14.98333637 04
| Epoch (UTC): | 25 May 2026 05:56:58 |
| Eccentricity: | 0.0003218 |
| inclination: | 69.9992° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 91.5961° |
| argument of perigee: | 268.6144° |
| revolutions per day: | 14.98333637 |
| mean anomaly at epoch: | 91.4646° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|