View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 16791U 26069.45770382 +.00000000 +00000-0 +26995-3 0 00000
2 16791 82.4609 142.7915 0013116 335.4439 24.6172 15.25714553 07
| Epoch (UTC): | 10 March 2026 10:59:05 |
| Eccentricity: | 0.0013116 |
| inclination: | 82.4609° |
| perigee height: | 480 km |
| apogee height: | 498 km |
| right ascension of ascending node: | 142.7915° |
| argument of perigee: | 335.4439° |
| revolutions per day: | 15.25714553 |
| mean anomaly at epoch: | 24.6172° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|