View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 58800U 26145.54750404 +.00000000 +00000-0 +66954-4 0 00005
2 58800 42.9996 90.9148 0000896 263.0529 97.0220 15.27567650 07
| Epoch (UTC): | 25 May 2026 13:08:24 |
| Eccentricity: | 0.0000896 |
| inclination: | 42.9996° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 90.9148° |
| argument of perigee: | 263.0529° |
| revolutions per day: | 15.27567650 |
| mean anomaly at epoch: | 97.0220° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|