View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 48991U 26145.49208589 +.00000000 +00000-0 -25351-3 0 00007
2 48991 87.9109 233.2895 0001871 99.4282 260.7060 13.16592645 03
| Epoch (UTC): | 25 May 2026 11:48:36 |
| Eccentricity: | 0.0001871 |
| inclination: | 87.9109° |
| perigee height: | 1196 km |
| apogee height: | 1199 km |
| right ascension of ascending node: | 233.2895° |
| argument of perigee: | 99.4282° |
| revolutions per day: | 13.16592645 |
| mean anomaly at epoch: | 260.7060° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|