View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 20775U 26042.09159661 +.00000000 +00000-0 +43112-3 0 00009
2 20775 82.9020 275.2138 0366834 103.1170 261.1253 14.88177151 08
| Epoch (UTC): | 11 February 2026 02:11:53 |
| Eccentricity: | 0.0366834 |
| inclination: | 82.9020° |
| perigee height: | 348 km |
| apogee height: | 860 km |
| right ascension of ascending node: | 275.2138° |
| argument of perigee: | 103.1170° |
| revolutions per day: | 14.88177151 |
| mean anomaly at epoch: | 261.1253° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|