View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 00012U 26107.20893631 +.00000000 +00000-0 +10339-3 0 00003
2 00012 32.8972 80.1213 1646286 142.2626 230.5692 11.48596347 02
| Epoch (UTC): | 17 April 2026 05:00:52 |
| Eccentricity: | 0.1646286 |
| inclination: | 32.8972° |
| perigee height: | 554 km |
| apogee height: | 3286 km |
| right ascension of ascending node: | 80.1213° |
| argument of perigee: | 142.2626° |
| revolutions per day: | 11.48596347 |
| mean anomaly at epoch: | 230.5692° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|