View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 25417U 26087.96135396 +.00000000 +00000-0 +47826-3 0 00007
2 25417 44.9929 259.4670 0003805 283.5105 76.5320 14.39887234 03
| Epoch (UTC): | 28 March 2026 23:04:20 |
| Eccentricity: | 0.0003805 |
| inclination: | 44.9929° |
| perigee height: | 756 km |
| apogee height: | 762 km |
| right ascension of ascending node: | 259.4670° |
| argument of perigee: | 283.5105° |
| revolutions per day: | 14.39887234 |
| mean anomaly at epoch: | 76.5320° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|