View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 23343U 26075.84850478 +.00000000 +00000-0 +65125-4 0 00005
2 23343 97.7098 106.3762 0006333 185.3521 347.4257 14.79416368 03
| Epoch (UTC): | 16 March 2026 20:21:50 |
| Eccentricity: | 0.0006333 |
| inclination: | 97.7098° |
| perigee height: | 627 km |
| apogee height: | 636 km |
| right ascension of ascending node: | 106.3762° |
| argument of perigee: | 185.3521° |
| revolutions per day: | 14.79416368 |
| mean anomaly at epoch: | 347.4257° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|