View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 16864U 26070.12001049 +.00000000 +00000-0 +92319-4 0 00008
2 16864 74.0291 309.9286 0032174 344.4988 15.5179 14.42275746 04
| Epoch (UTC): | 11 March 2026 02:52:48 |
| Eccentricity: | 0.0032174 |
| inclination: | 74.0291° |
| perigee height: | 728 km |
| apogee height: | 774 km |
| right ascension of ascending node: | 309.9286° |
| argument of perigee: | 344.4988° |
| revolutions per day: | 14.42275746 |
| mean anomaly at epoch: | 15.5179° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|