View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 66863U 26145.40860065 +.00000000 +00000-0 +10314-2 0 00000
2 66863 42.9999 269.7701 0001217 226.0524 134.0228 15.27597941 07
| Epoch (UTC): | 25 May 2026 09:48:23 |
| Eccentricity: | 0.0001217 |
| inclination: | 42.9999° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 269.7701° |
| argument of perigee: | 226.0524° |
| revolutions per day: | 15.27597941 |
| mean anomaly at epoch: | 134.0228° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|