View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 22829U 26053.69082926 +.00000000 +00000-0 +51595-4 0 00003
2 22829 98.6795 120.8607 0009772 13.2292 346.9146 14.31883452 09
| Epoch (UTC): | 22 February 2026 16:34:47 |
| Eccentricity: | 0.0009772 |
| inclination: | 98.6795° |
| perigee height: | 778 km |
| apogee height: | 792 km |
| right ascension of ascending node: | 120.8607° |
| argument of perigee: | 13.2292° |
| revolutions per day: | 14.31883452 |
| mean anomaly at epoch: | 346.9146° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|