View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 65404U 26145.54521213 +.00000000 +00000-0 +53176-3 0 00008
2 65404 53.1596 245.1473 0001348 87.7606 272.3551 15.34396006 08
| Epoch (UTC): | 25 May 2026 13:05:06 |
| Eccentricity: | 0.0001348 |
| inclination: | 53.1596° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 245.1473° |
| argument of perigee: | 87.7606° |
| revolutions per day: | 15.34396006 |
| mean anomaly at epoch: | 272.3551° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|