View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 57979U 26144.74494250 +.00000000 +00000-0 -18503-5 0 00005
2 57979 43.0000 281.2797 0001086 278.4119 81.6609 15.27573103 03
| Epoch (UTC): | 24 May 2026 17:52:43 |
| Eccentricity: | 0.0001086 |
| inclination: | 43.0000° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 281.2797° |
| argument of perigee: | 278.4119° |
| revolutions per day: | 15.27573103 |
| mean anomaly at epoch: | 81.6609° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|