View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 58125U 26145.18675979 +.00000000 +00000-0 +91146-4 0 00009
2 58125 43.0025 57.3006 0001112 256.8746 103.1982 15.27580299 03
| Epoch (UTC): | 25 May 2026 04:28:56 |
| Eccentricity: | 0.0001112 |
| inclination: | 43.0025° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 57.3006° |
| argument of perigee: | 256.8746° |
| revolutions per day: | 15.27580299 |
| mean anomaly at epoch: | 103.1982° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|