View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 58931U 26145.19769229 +.00000000 +00000-0 -63992-4 0 00006
2 58931 53.1626 314.1353 0001447 95.1257 264.9909 15.30207503 01
| Epoch (UTC): | 25 May 2026 04:44:40 |
| Eccentricity: | 0.0001447 |
| inclination: | 53.1626° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 314.1353° |
| argument of perigee: | 95.1257° |
| revolutions per day: | 15.30207503 |
| mean anomaly at epoch: | 264.9909° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|