View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 23480U 26073.93130877 +.00000000 +00000-0 +16527-1 0 00008
2 23480 64.7056 283.0631 0216321 153.1233 320.6019 11.46081799 00
| Epoch (UTC): | 14 March 2026 22:21:05 |
| Eccentricity: | 0.0216321 |
| inclination: | 64.7056° |
| perigee height: | 1752 km |
| apogee height: | 2111 km |
| right ascension of ascending node: | 283.0631° |
| argument of perigee: | 153.1233° |
| revolutions per day: | 11.46081799 |
| mean anomaly at epoch: | 320.6019° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|