View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 28945U 26144.41178648 +.00000000 +00000-0 +00000-0 0 00007
2 28945 0.5036 86.8966 0004933 333.1752 299.9725 1.00273252 05
| Epoch (UTC): | 24 May 2026 09:52:58 |
| Eccentricity: | 0.0004933 |
| inclination: | 0.5036° |
| perigee height: | 35765 km |
| apogee height: | 35807 km |
| right ascension of ascending node: | 86.8966° |
| argument of perigee: | 333.1752° |
| revolutions per day: | 1.00273252 |
| mean anomaly at epoch: | 299.9725° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|