View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 48239U 26145.39756647 +.00000000 +00000-0 +65602-3 0 00006
2 48239 87.8945 294.2408 0002023 99.0924 261.0435 13.14501562 07
| Epoch (UTC): | 25 May 2026 09:32:29 |
| Eccentricity: | 0.0002023 |
| inclination: | 87.8945° |
| perigee height: | 1204 km |
| apogee height: | 1207 km |
| right ascension of ascending node: | 294.2408° |
| argument of perigee: | 99.0924° |
| revolutions per day: | 13.14501562 |
| mean anomaly at epoch: | 261.0435° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|