View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 23106U 26088.14496451 +.00000000 +00000-0 +26302-3 0 00009
2 23106 81.9589 339.9296 0113108 26.3609 334.3293 14.76480232 09
| Epoch (UTC): | 29 March 2026 03:28:44 |
| Eccentricity: | 0.0113108 |
| inclination: | 81.9589° |
| perigee height: | 561 km |
| apogee height: | 720 km |
| right ascension of ascending node: | 339.9296° |
| argument of perigee: | 26.3609° |
| revolutions per day: | 14.76480232 |
| mean anomaly at epoch: | 334.3293° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|