View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 16791U 26067.68689642 +.00000000 +00000-0 +35564-3 0 00003
2 16791 82.4606 144.5761 0013265 341.9806 18.0960 15.25688429 02
| Epoch (UTC): | 08 March 2026 16:29:07 |
| Eccentricity: | 0.0013265 |
| inclination: | 82.4606° |
| perigee height: | 480 km |
| apogee height: | 498 km |
| right ascension of ascending node: | 144.5761° |
| argument of perigee: | 341.9806° |
| revolutions per day: | 15.25688429 |
| mean anomaly at epoch: | 18.0960° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|