View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 16117U 26145.63284689 +.00000000 +00000-0 +00000-0 0 00003
2 16117 14.3028 346.4731 0004764 109.4070 263.6822 0.98987855 04
| Epoch (UTC): | 25 May 2026 15:11:17 |
| Eccentricity: | 0.0004764 |
| inclination: | 14.3028° |
| perigee height: | 36130 km |
| apogee height: | 36171 km |
| right ascension of ascending node: | 346.4731° |
| argument of perigee: | 109.4070° |
| revolutions per day: | 0.98987855 |
| mean anomaly at epoch: | 263.6822° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|