View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 68175U 26144.77686264 +.00000000 +00000-0 +77386-3 0 00007
2 68175 53.1584 272.5350 0000795 105.7376 254.3715 15.34400691 09
| Epoch (UTC): | 24 May 2026 18:38:40 |
| Eccentricity: | 0.0000795 |
| inclination: | 53.1584° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 272.5350° |
| argument of perigee: | 105.7376° |
| revolutions per day: | 15.34400691 |
| mean anomaly at epoch: | 254.3715° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|