View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 57148U 26145.48022076 +.00000000 +00000-0 +13548-4 0 00000
2 57148 43.0021 189.9887 0001021 289.6093 70.4648 15.27574719 05
| Epoch (UTC): | 25 May 2026 11:31:31 |
| Eccentricity: | 0.0001021 |
| inclination: | 43.0021° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 189.9887° |
| argument of perigee: | 289.6093° |
| revolutions per day: | 15.27574719 |
| mean anomaly at epoch: | 70.4648° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|