View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 58595U 26145.20990318 +.00000000 +00000-0 -88243-5 0 00006
2 58595 43.0003 96.7056 0001327 270.4942 89.5757 15.27579397 04
| Epoch (UTC): | 25 May 2026 05:02:15 |
| Eccentricity: | 0.0001327 |
| inclination: | 43.0003° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 96.7056° |
| argument of perigee: | 270.4942° |
| revolutions per day: | 15.27579397 |
| mean anomaly at epoch: | 89.5757° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|