View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 48974U 26145.49920225 +.00000000 +00000-0 +55503-4 0 00008
2 48974 87.9100 233.2894 0002097 99.5621 260.5747 13.16596865 01
| Epoch (UTC): | 25 May 2026 11:58:51 |
| Eccentricity: | 0.0002097 |
| inclination: | 87.9100° |
| perigee height: | 1196 km |
| apogee height: | 1199 km |
| right ascension of ascending node: | 233.2894° |
| argument of perigee: | 99.5621° |
| revolutions per day: | 13.16596865 |
| mean anomaly at epoch: | 260.5747° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|