View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 61920U 26145.46768397 +.00000000 +00000-0 +55791-3 0 00009
2 61920 42.9999 208.1927 0001228 272.4512 87.6199 15.27590578 06
| Epoch (UTC): | 25 May 2026 11:13:27 |
| Eccentricity: | 0.0001228 |
| inclination: | 42.9999° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 208.1927° |
| argument of perigee: | 272.4512° |
| revolutions per day: | 15.27590578 |
| mean anomaly at epoch: | 87.6199° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|