View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 39765U 26156.58094457 +.00000000 +00000-0 +12128-3 0 00002
2 39765 82.4496 260.2590 0231862 29.1650 332.2172 12.82902530 06
| Epoch (UTC): | 05 June 2026 13:56:33 |
| Eccentricity: | 0.0231862 |
| inclination: | 82.4496° |
| perigee height: | 1151 km |
| apogee height: | 1509 km |
| right ascension of ascending node: | 260.2590° |
| argument of perigee: | 29.1650° |
| revolutions per day: | 12.82902530 |
| mean anomaly at epoch: | 332.2172° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|