View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 58515U 26145.48305941 +.00000000 +00000-0 -20045-4 0 00005
2 58515 43.0023 157.4787 0001238 284.3283 75.7431 15.27572268 03
| Epoch (UTC): | 25 May 2026 11:35:36 |
| Eccentricity: | 0.0001238 |
| inclination: | 43.0023° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 157.4787° |
| argument of perigee: | 284.3283° |
| revolutions per day: | 15.27572268 |
| mean anomaly at epoch: | 75.7431° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|