View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 65593U 26145.45716293 +.00000000 +00000-0 +35393-3 0 00002
2 65593 97.4520 213.9726 0001430 192.4565 167.6627 15.05654341 06
| Epoch (UTC): | 25 May 2026 10:58:18 |
| Eccentricity: | 0.0001430 |
| inclination: | 97.4520° |
| perigee height: | 549 km |
| apogee height: | 550 km |
| right ascension of ascending node: | 213.9726° |
| argument of perigee: | 192.4565° |
| revolutions per day: | 15.05654341 |
| mean anomaly at epoch: | 167.6627° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|