View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 68372U 26144.14419807 +.00000000 +00000-0 +29394-3 0 00000
2 68372 82.2960 40.0454 0007929 131.9233 228.2698 15.55722428 09
| Epoch (UTC): | 24 May 2026 03:27:38 |
| Eccentricity: | 0.0007929 |
| inclination: | 82.2960° |
| perigee height: | 395 km |
| apogee height: | 405 km |
| right ascension of ascending node: | 40.0454° |
| argument of perigee: | 131.9233° |
| revolutions per day: | 15.55722428 |
| mean anomaly at epoch: | 228.2698° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|