View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 61013U 26145.59981273 +.00000000 +00000-0 +19099-3 0 00007
2 61013 49.9922 186.8297 0005347 36.7326 323.3978 14.84152829 04
| Epoch (UTC): | 25 May 2026 14:23:43 |
| Eccentricity: | 0.0005347 |
| inclination: | 49.9922° |
| perigee height: | 613 km |
| apogee height: | 620 km |
| right ascension of ascending node: | 186.8297° |
| argument of perigee: | 36.7326° |
| revolutions per day: | 14.84152829 |
| mean anomaly at epoch: | 323.3978° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|