View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 57196U 26145.55857757 +.00000000 +00000-0 +42549-3 0 00005
2 57196 97.5101 212.2898 0009173 155.2959 204.8723 15.31219001 00
| Epoch (UTC): | 25 May 2026 13:24:21 |
| Eccentricity: | 0.0009173 |
| inclination: | 97.5101° |
| perigee height: | 466 km |
| apogee height: | 478 km |
| right ascension of ascending node: | 212.2898° |
| argument of perigee: | 155.2959° |
| revolutions per day: | 15.31219001 |
| mean anomaly at epoch: | 204.8723° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|