View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 12088U 26088.19044433 +.00000000 +00000-0 -31046-4 0 00003
2 12088 82.9393 118.2216 0050300 89.2197 271.4724 13.77329591 04
| Epoch (UTC): | 29 March 2026 04:34:14 |
| Eccentricity: | 0.0050300 |
| inclination: | 82.9393° |
| perigee height: | 936 km |
| apogee height: | 1010 km |
| right ascension of ascending node: | 118.2216° |
| argument of perigee: | 89.2197° |
| revolutions per day: | 13.77329591 |
| mean anomaly at epoch: | 271.4724° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|