View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 59379U 26145.57727175 +.00000000 +00000-0 +16619-3 0 00001
2 59379 53.1605 258.5139 0001377 93.3648 266.7511 15.30191038 08
| Epoch (UTC): | 25 May 2026 13:51:16 |
| Eccentricity: | 0.0001377 |
| inclination: | 53.1605° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 258.5139° |
| argument of perigee: | 93.3648° |
| revolutions per day: | 15.30191038 |
| mean anomaly at epoch: | 266.7511° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|