View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 39763U 26106.88305729 +.00000000 +00000-0 +32818-3 0 00003
2 39763 82.4463 147.3112 0020769 203.8809 156.1309 12.42978453 00
| Epoch (UTC): | 16 April 2026 21:11:36 |
| Eccentricity: | 0.0020769 |
| inclination: | 82.4463° |
| perigee height: | 1478 km |
| apogee height: | 1510 km |
| right ascension of ascending node: | 147.3112° |
| argument of perigee: | 203.8809° |
| revolutions per day: | 12.42978453 |
| mean anomaly at epoch: | 156.1309° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|