View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 65467U 26144.81098868 +.00000000 +00000-0 +51453-3 0 00007
2 65467 53.1580 264.9303 0000891 81.6941 278.4161 15.30212788 02
| Epoch (UTC): | 24 May 2026 19:27:49 |
| Eccentricity: | 0.0000891 |
| inclination: | 53.1580° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 264.9303° |
| argument of perigee: | 81.6941° |
| revolutions per day: | 15.30212788 |
| mean anomaly at epoch: | 278.4161° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|