View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 58352U 26145.34487985 +.00000000 +00000-0 +12841-4 0 00002
2 58352 43.0018 277.4521 0001163 264.3866 95.6853 15.27580575 06
| Epoch (UTC): | 25 May 2026 08:16:37 |
| Eccentricity: | 0.0001163 |
| inclination: | 43.0018° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 277.4521° |
| argument of perigee: | 264.3866° |
| revolutions per day: | 15.27580575 |
| mean anomaly at epoch: | 95.6853° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|