View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 58061U 26145.43966984 +.00000000 +00000-0 +58298-4 0 00006
2 58061 43.0048 287.8044 0001575 264.7170 95.3502 15.27578332 06
| Epoch (UTC): | 25 May 2026 10:33:07 |
| Eccentricity: | 0.0001575 |
| inclination: | 43.0048° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 287.8044° |
| argument of perigee: | 264.7170° |
| revolutions per day: | 15.27578332 |
| mean anomaly at epoch: | 95.3502° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|