View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 58031U 26145.13746359 +.00000000 +00000-0 +37129-4 0 00002
2 58031 53.1619 92.7040 0001259 93.7340 266.3807 15.34393741 01
| Epoch (UTC): | 25 May 2026 03:17:56 |
| Eccentricity: | 0.0001259 |
| inclination: | 53.1619° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 92.7040° |
| argument of perigee: | 93.7340° |
| revolutions per day: | 15.34393741 |
| mean anomaly at epoch: | 266.3807° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|