View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 62119U 26145.17348294 +.00000000 +00000-0 +77656-3 0 00002
2 62119 42.9992 61.0049 0001568 273.5643 86.5029 15.27617786 06
| Epoch (UTC): | 25 May 2026 04:09:48 |
| Eccentricity: | 0.0001568 |
| inclination: | 42.9992° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 61.0049° |
| argument of perigee: | 273.5643° |
| revolutions per day: | 15.27617786 |
| mean anomaly at epoch: | 86.5029° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|