View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 48057U 26145.43584199 +.00000000 +00000-0 -42359-3 0 00005
2 48057 87.8945 324.7517 0001621 93.0871 267.0443 13.13468162 05
| Epoch (UTC): | 25 May 2026 10:27:36 |
| Eccentricity: | 0.0001621 |
| inclination: | 87.8945° |
| perigee height: | 1209 km |
| apogee height: | 1211 km |
| right ascension of ascending node: | 324.7517° |
| argument of perigee: | 93.0871° |
| revolutions per day: | 13.13468162 |
| mean anomaly at epoch: | 267.0443° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|