View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 65257U 26088.11567625 +.00000000 +00000-0 -80536-3 0 00001
2 65257 97.6041 132.1503 0001361 103.3233 256.8146 15.05622334 08
| Epoch (UTC): | 29 March 2026 02:46:34 |
| Eccentricity: | 0.0001361 |
| inclination: | 97.6041° |
| perigee height: | 549 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 132.1503° |
| argument of perigee: | 103.3233° |
| revolutions per day: | 15.05622334 |
| mean anomaly at epoch: | 256.8146° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|