View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 35683U 26032.49823240 +.00000000 +00000-0 +21620-3 0 00007
2 35683 97.8592 170.9847 0001410 76.4500 283.6866 14.75763498 04
| Epoch (UTC): | 01 February 2026 11:57:27 |
| Eccentricity: | 0.0001410 |
| inclination: | 97.8592° |
| perigee height: | 642 km |
| apogee height: | 644 km |
| right ascension of ascending node: | 170.9847° |
| argument of perigee: | 76.4500° |
| revolutions per day: | 14.75763498 |
| mean anomaly at epoch: | 283.6866° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|