View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 16612U 26075.72309994 +.00000000 +00000-0 +48642-4 0 00000
2 16612 82.5189 176.2954 0017708 43.4426 316.8183 14.86688050 07
| Epoch (UTC): | 16 March 2026 17:21:15 |
| Eccentricity: | 0.0017708 |
| inclination: | 82.5189° |
| perigee height: | 596 km |
| apogee height: | 621 km |
| right ascension of ascending node: | 176.2954° |
| argument of perigee: | 43.4426° |
| revolutions per day: | 14.86688050 |
| mean anomaly at epoch: | 316.8183° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|