View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 56137U 26145.07798098 +.00000000 +00000-0 +45954-4 0 00002
2 56137 43.0055 75.5025 0001408 258.6529 101.4164 15.27572959 04
| Epoch (UTC): | 25 May 2026 01:52:17 |
| Eccentricity: | 0.0001408 |
| inclination: | 43.0055° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 75.5025° |
| argument of perigee: | 258.6529° |
| revolutions per day: | 15.27572959 |
| mean anomaly at epoch: | 101.4164° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|