View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 60493U 26145.46875412 +.00000000 +00000-0 +30768-3 0 00007
2 60493 97.3790 226.8905 0001720 276.8784 83.2260 15.29397676 09
| Epoch (UTC): | 25 May 2026 11:15:00 |
| Eccentricity: | 0.0001720 |
| inclination: | 97.3790° |
| perigee height: | 476 km |
| apogee height: | 479 km |
| right ascension of ascending node: | 226.8905° |
| argument of perigee: | 276.8784° |
| revolutions per day: | 15.29397676 |
| mean anomaly at epoch: | 83.2260° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|