View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 59888U 26145.11924486 +.00000000 +00000-0 +27643-3 0 00009
2 59888 43.0013 53.9491 0001100 268.1823 91.8903 15.27592029 06
| Epoch (UTC): | 25 May 2026 02:51:42 |
| Eccentricity: | 0.0001100 |
| inclination: | 43.0013° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 53.9491° |
| argument of perigee: | 268.1823° |
| revolutions per day: | 15.27592029 |
| mean anomaly at epoch: | 91.8903° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|