View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 21423U 26021.42149188 +.00000000 +00000-0 +88077-4 0 00007
2 21423 82.4920 264.5167 0018073 40.3443 319.9108 14.81781393 03
| Epoch (UTC): | 21 January 2026 10:06:56 |
| Eccentricity: | 0.0018073 |
| inclination: | 82.4920° |
| perigee height: | 611 km |
| apogee height: | 636 km |
| right ascension of ascending node: | 264.5167° |
| argument of perigee: | 40.3443° |
| revolutions per day: | 14.81781393 |
| mean anomaly at epoch: | 319.9108° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|