View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 41579U 26145.61882328 +.00000000 +00000-0 +54186-4 0 00003
2 41579 99.1884 154.8323 0001104 87.8314 272.2969 13.85908234 00
| Epoch (UTC): | 25 May 2026 14:51:06 |
| Eccentricity: | 0.0001104 |
| inclination: | 99.1884° |
| perigee height: | 942 km |
| apogee height: | 944 km |
| right ascension of ascending node: | 154.8323° |
| argument of perigee: | 87.8314° |
| revolutions per day: | 13.85908234 |
| mean anomaly at epoch: | 272.2969° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|