View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 40034U 26150.41511132 +.00000000 +00000-0 +53113-3 0 00002
2 40034 97.7756 306.4552 0044629 114.8962 245.6905 14.90771539 02
| Epoch (UTC): | 30 May 2026 09:57:45 |
| Eccentricity: | 0.0044629 |
| inclination: | 97.7756° |
| perigee height: | 564 km |
| apogee height: | 627 km |
| right ascension of ascending node: | 306.4552° |
| argument of perigee: | 114.8962° |
| revolutions per day: | 14.90771539 |
| mean anomaly at epoch: | 245.6905° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|