View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 49122U 26145.60906302 +.00000000 +00000-0 +10803-3 0 00000
2 49122 98.2606 220.0795 0002321 72.4614 287.6838 14.57680708 06
| Epoch (UTC): | 25 May 2026 14:37:03 |
| Eccentricity: | 0.0002321 |
| inclination: | 98.2606° |
| perigee height: | 699 km |
| apogee height: | 702 km |
| right ascension of ascending node: | 220.0795° |
| argument of perigee: | 72.4614° |
| revolutions per day: | 14.57680708 |
| mean anomaly at epoch: | 287.6838° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|