View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 65111U 26145.62421076 +.00000000 +00000-0 +12144-3 0 00008
2 65111 50.0002 46.2761 0011096 29.5341 330.6156 13.29321747 03
| Epoch (UTC): | 25 May 2026 14:58:51 |
| Eccentricity: | 0.0011096 |
| inclination: | 50.0002° |
| perigee height: | 1141 km |
| apogee height: | 1158 km |
| right ascension of ascending node: | 46.2761° |
| argument of perigee: | 29.5341° |
| revolutions per day: | 13.29321747 |
| mean anomaly at epoch: | 330.6156° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|