View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 62150U 26145.51250986 +.00000000 +00000-0 +26769-3 0 00004
2 62150 42.9991 83.8562 0000791 276.1203 83.9558 15.27599010 07
| Epoch (UTC): | 25 May 2026 12:18:00 |
| Eccentricity: | 0.0000791 |
| inclination: | 42.9991° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 83.8562° |
| argument of perigee: | 276.1203° |
| revolutions per day: | 15.27599010 |
| mean anomaly at epoch: | 83.9558° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|