View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 33412U 26159.24531131 +.00000000 +00000-0 +14272-3 0 00008
2 33412 97.8291 17.6678 0014291 300.7559 59.2260 15.06893314 06
| Epoch (UTC): | 08 June 2026 05:53:14 |
| Eccentricity: | 0.0014291 |
| inclination: | 97.8291° |
| perigee height: | 536 km |
| apogee height: | 556 km |
| right ascension of ascending node: | 17.6678° |
| argument of perigee: | 300.7559° |
| revolutions per day: | 15.06893314 |
| mean anomaly at epoch: | 59.2260° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|