View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 65875U 26145.14162163 +.00000000 +00000-0 +89766-3 0 00005
2 65875 53.1603 298.8594 0001172 102.3052 257.8082 15.34392581 03
| Epoch (UTC): | 25 May 2026 03:23:56 |
| Eccentricity: | 0.0001172 |
| inclination: | 53.1603° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 298.8594° |
| argument of perigee: | 102.3052° |
| revolutions per day: | 15.34392581 |
| mean anomaly at epoch: | 257.8082° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|