View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 38782U 26032.51511778 +.00000000 +00000-0 +26683-3 0 00007
2 38782 97.6007 15.9331 0017006 325.1076 34.9021 14.79695131 04
| Epoch (UTC): | 01 February 2026 12:21:46 |
| Eccentricity: | 0.0017006 |
| inclination: | 97.6007° |
| perigee height: | 618 km |
| apogee height: | 642 km |
| right ascension of ascending node: | 15.9331° |
| argument of perigee: | 325.1076° |
| revolutions per day: | 14.79695131 |
| mean anomaly at epoch: | 34.9021° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|