View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 16953U 26075.59679943 +.00000000 +00000-0 +77503-4 0 00005
2 16953 74.0117 147.0815 0012880 322.1915 37.8333 14.38819867 06
| Epoch (UTC): | 16 March 2026 14:19:23 |
| Eccentricity: | 0.0012880 |
| inclination: | 74.0117° |
| perigee height: | 753 km |
| apogee height: | 772 km |
| right ascension of ascending node: | 147.0815° |
| argument of perigee: | 322.1915° |
| revolutions per day: | 14.38819867 |
| mean anomaly at epoch: | 37.8333° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|