View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 39421U 26032.45821008 +.00000000 +00000-0 +33604-3 0 00002
2 39421 97.6904 3.2543 0029901 187.5936 172.4841 15.03748007 05
| Epoch (UTC): | 01 February 2026 10:59:49 |
| Eccentricity: | 0.0029901 |
| inclination: | 97.6904° |
| perigee height: | 535 km |
| apogee height: | 576 km |
| right ascension of ascending node: | 3.2543° |
| argument of perigee: | 187.5936° |
| revolutions per day: | 15.03748007 |
| mean anomaly at epoch: | 172.4841° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|