View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 32294U 26150.50806477 +.00000000 +00000-0 +00000-0 0 00004
2 32294 5.2088 73.7109 0003779 350.5184 31.7739 1.00271555 00
| Epoch (UTC): | 30 May 2026 12:11:36 |
| Eccentricity: | 0.0003779 |
| inclination: | 5.2088° |
| perigee height: | 35771 km |
| apogee height: | 35803 km |
| right ascension of ascending node: | 73.7109° |
| argument of perigee: | 350.5184° |
| revolutions per day: | 1.00271555 |
| mean anomaly at epoch: | 31.7739° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|