View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 36122U 26141.26419566 +.00000000 +00000-0 -73602-3 0 00002
2 36122 100.4020 95.5292 0006973 298.9262 61.1152 13.16437287 06
| Epoch (UTC): | 21 May 2026 06:20:26 |
| Eccentricity: | 0.0006973 |
| inclination: | 100.4020° |
| perigee height: | 1193 km |
| apogee height: | 1204 km |
| right ascension of ascending node: | 95.5292° |
| argument of perigee: | 298.9262° |
| revolutions per day: | 13.16437287 |
| mean anomaly at epoch: | 61.1152° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|