View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 00051U 26041.15108088 +.00000000 +00000-0 -42383-3 0 00007
2 00051 47.2130 82.4489 0110274 179.9077 180.1747 12.18379064 04
| Epoch (UTC): | 10 February 2026 03:37:33 |
| Eccentricity: | 0.0110274 |
| inclination: | 47.2130° |
| perigee height: | 1512 km |
| apogee height: | 1688 km |
| right ascension of ascending node: | 82.4489° |
| argument of perigee: | 179.9077° |
| revolutions per day: | 12.18379064 |
| mean anomaly at epoch: | 180.1747° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|