View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 65425U 26145.24319551 +.00000000 +00000-0 +55331-3 0 00003
2 65425 53.1590 236.8542 0001184 81.2051 278.9084 15.31724009 08
| Epoch (UTC): | 25 May 2026 05:50:12 |
| Eccentricity: | 0.0001184 |
| inclination: | 53.1590° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 236.8542° |
| argument of perigee: | 81.2051° |
| revolutions per day: | 15.31724009 |
| mean anomaly at epoch: | 278.9084° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|