View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 48908U 26145.51152150 +.00000000 +00000-0 +33758-3 0 00009
2 48908 97.7020 336.3021 0004686 80.9914 279.1871 15.58274204 02
| Epoch (UTC): | 25 May 2026 12:16:35 |
| Eccentricity: | 0.0004686 |
| inclination: | 97.7020° |
| perigee height: | 389 km |
| apogee height: | 396 km |
| right ascension of ascending node: | 336.3021° |
| argument of perigee: | 80.9914° |
| revolutions per day: | 15.58274204 |
| mean anomaly at epoch: | 279.1871° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|