View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 21422U 26038.86555220 +.00000000 +00000-0 +19654-3 0 00004
2 21422 82.4963 112.4452 0013206 154.2424 205.9461 14.99989456 09
| Epoch (UTC): | 07 February 2026 20:46:23 |
| Eccentricity: | 0.0013206 |
| inclination: | 82.4963° |
| perigee height: | 558 km |
| apogee height: | 576 km |
| right ascension of ascending node: | 112.4452° |
| argument of perigee: | 154.2424° |
| revolutions per day: | 14.99989456 |
| mean anomaly at epoch: | 205.9461° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|