View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 48242U 26145.64732330 +.00000000 +00000-0 +23319-3 0 00000
2 48242 87.8950 294.1929 0002035 104.3032 255.8324 13.14500786 02
| Epoch (UTC): | 25 May 2026 15:32:08 |
| Eccentricity: | 0.0002035 |
| inclination: | 87.8950° |
| perigee height: | 1204 km |
| apogee height: | 1207 km |
| right ascension of ascending node: | 294.1929° |
| argument of perigee: | 104.3032° |
| revolutions per day: | 13.14500786 |
| mean anomaly at epoch: | 255.8324° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|