View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 20104U 26066.14588265 +.00000000 +00000-0 +63869-4 0 00005
2 20104 82.9595 327.4881 0042125 261.9822 97.6554 13.77617327 04
| Epoch (UTC): | 07 March 2026 03:30:04 |
| Eccentricity: | 0.0042125 |
| inclination: | 82.9595° |
| perigee height: | 941 km |
| apogee height: | 1003 km |
| right ascension of ascending node: | 327.4881° |
| argument of perigee: | 261.9822° |
| revolutions per day: | 13.77617327 |
| mean anomaly at epoch: | 97.6554° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|