View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 12849U 26022.17939701 +.00000000 +00000-0 +21197-3 0 00009
2 12849 82.4866 268.3591 0869127 222.4393 130.6332 13.57877678 09
| Epoch (UTC): | 22 January 2026 04:18:19 |
| Eccentricity: | 0.0869127 |
| inclination: | 82.4866° |
| perigee height: | 398 km |
| apogee height: | 1688 km |
| right ascension of ascending node: | 268.3591° |
| argument of perigee: | 222.4393° |
| revolutions per day: | 13.57877678 |
| mean anomaly at epoch: | 130.6332° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|