View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 22825U 26069.12657844 +.00000000 +00000-0 +69774-4 0 00009
2 22825 98.6981 136.5370 0008926 37.7276 322.4531 14.30913239 09
| Epoch (UTC): | 10 March 2026 03:02:16 |
| Eccentricity: | 0.0008926 |
| inclination: | 98.6981° |
| perigee height: | 782 km |
| apogee height: | 795 km |
| right ascension of ascending node: | 136.5370° |
| argument of perigee: | 37.7276° |
| revolutions per day: | 14.30913239 |
| mean anomaly at epoch: | 322.4531° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|