View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 60110U 26145.13045330 +.00000000 +00000-0 -21151-4 0 00003
2 60110 53.1620 41.7957 0001150 122.3536 237.7576 15.30187924 06
| Epoch (UTC): | 25 May 2026 03:07:51 |
| Eccentricity: | 0.0001150 |
| inclination: | 53.1620° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 41.7957° |
| argument of perigee: | 122.3536° |
| revolutions per day: | 15.30187924 |
| mean anomaly at epoch: | 237.7576° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|