View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 68179U 26145.35790603 +.00000000 +00000-0 +78731-3 0 00004
2 68179 53.1585 270.4779 0001066 105.6652 254.4470 15.38850252 09
| Epoch (UTC): | 25 May 2026 08:35:23 |
| Eccentricity: | 0.0001066 |
| inclination: | 53.1585° |
| perigee height: | 449 km |
| apogee height: | 450 km |
| right ascension of ascending node: | 270.4779° |
| argument of perigee: | 105.6652° |
| revolutions per day: | 15.38850252 |
| mean anomaly at epoch: | 254.4470° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|