View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 02422U 26100.13957257 +.00000000 +00000-0 +10731-3 0 00006
2 02422 98.2349 256.7157 0111071 55.1568 306.0010 14.46726365 05
| Epoch (UTC): | 10 April 2026 03:20:59 |
| Eccentricity: | 0.0111071 |
| inclination: | 98.2349° |
| perigee height: | 657 km |
| apogee height: | 815 km |
| right ascension of ascending node: | 256.7157° |
| argument of perigee: | 55.1568° |
| revolutions per day: | 14.46726365 |
| mean anomaly at epoch: | 306.0010° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|