View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 02016U 26106.03538674 +.00000000 +00000-0 +90029-4 0 00007
2 02016 34.0892 230.3273 1157887 8.5745 353.2962 12.66483602 01
| Epoch (UTC): | 16 April 2026 00:50:57 |
| Eccentricity: | 0.1157887 |
| inclination: | 34.0892° |
| perigee height: | 496 km |
| apogee height: | 2296 km |
| right ascension of ascending node: | 230.3273° |
| argument of perigee: | 8.5745° |
| revolutions per day: | 12.66483602 |
| mean anomaly at epoch: | 353.2962° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|