View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 59880U 26145.43991559 +.00000000 +00000-0 +54771-4 0 00004
2 59880 43.0008 204.5882 0001472 275.5307 84.5377 15.27577478 06
| Epoch (UTC): | 25 May 2026 10:33:28 |
| Eccentricity: | 0.0001472 |
| inclination: | 43.0008° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 204.5882° |
| argument of perigee: | 275.5307° |
| revolutions per day: | 15.27577478 |
| mean anomaly at epoch: | 84.5377° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|