View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 16792U 26039.57500328 +.00000000 +00000-0 +56597-4 0 00004
2 16792 82.4815 107.6956 0022218 327.5189 32.4658 14.85562003 01
| Epoch (UTC): | 08 February 2026 13:48:00 |
| Eccentricity: | 0.0022218 |
| inclination: | 82.4815° |
| perigee height: | 596 km |
| apogee height: | 627 km |
| right ascension of ascending node: | 107.6956° |
| argument of perigee: | 327.5189° |
| revolutions per day: | 14.85562003 |
| mean anomaly at epoch: | 32.4658° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|