View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 48799U 26145.39349706 +.00000000 +00000-0 +52968-3 0 00002
2 48799 87.8990 263.7394 0001466 86.6349 273.4949 13.15547658 00
| Epoch (UTC): | 25 May 2026 09:26:38 |
| Eccentricity: | 0.0001466 |
| inclination: | 87.8990° |
| perigee height: | 1201 km |
| apogee height: | 1203 km |
| right ascension of ascending node: | 263.7394° |
| argument of perigee: | 86.6349° |
| revolutions per day: | 13.15547658 |
| mean anomaly at epoch: | 273.4949° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|