View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 65951U 26145.37274486 +.00000000 +00000-0 -38719-4 0 00001
2 65951 51.9009 23.9714 0001365 91.3062 268.8057 14.79964068 04
| Epoch (UTC): | 25 May 2026 08:56:45 |
| Eccentricity: | 0.0001365 |
| inclination: | 51.9009° |
| perigee height: | 628 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 23.9714° |
| argument of perigee: | 91.3062° |
| revolutions per day: | 14.79964068 |
| mean anomaly at epoch: | 268.8057° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|