View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 59085U 26145.23896163 +.00000000 +00000-0 +58287-4 0 00000
2 59085 42.9988 224.1264 0001269 271.5625 88.5082 15.27575382 02
| Epoch (UTC): | 25 May 2026 05:44:06 |
| Eccentricity: | 0.0001269 |
| inclination: | 42.9988° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 224.1264° |
| argument of perigee: | 271.5625° |
| revolutions per day: | 15.27575382 |
| mean anomaly at epoch: | 88.5082° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|