View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 32783U 26032.54760470 +.00000000 +00000-0 +96495-4 0 00009
2 32783 97.7859 85.7660 0011530 185.5521 174.5565 14.79029917 01
| Epoch (UTC): | 01 February 2026 13:08:33 |
| Eccentricity: | 0.0011530 |
| inclination: | 97.7859° |
| perigee height: | 624 km |
| apogee height: | 640 km |
| right ascension of ascending node: | 85.7660° |
| argument of perigee: | 185.5521° |
| revolutions per day: | 14.79029917 |
| mean anomaly at epoch: | 174.5565° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|