View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 21965U 26158.48438892 +.00000000 +00000-0 +15144-3 0 00002
2 21965 19.6742 226.3779 1357180 121.1309 252.9257 12.22504697 02
| Epoch (UTC): | 07 June 2026 11:37:31 |
| Eccentricity: | 0.1357180 |
| inclination: | 19.6742° |
| perigee height: | 501 km |
| apogee height: | 2662 km |
| right ascension of ascending node: | 226.3779° |
| argument of perigee: | 121.1309° |
| revolutions per day: | 12.22504697 |
| mean anomaly at epoch: | 252.9257° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|