View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 65045U 26145.59554523 +.00000000 +00000-0 +91329-4 0 00007
2 65045 49.9986 346.7667 0000480 44.2447 315.8463 13.29324239 01
| Epoch (UTC): | 25 May 2026 14:17:35 |
| Eccentricity: | 0.0000480 |
| inclination: | 49.9986° |
| perigee height: | 1149 km |
| apogee height: | 1150 km |
| right ascension of ascending node: | 346.7667° |
| argument of perigee: | 44.2447° |
| revolutions per day: | 13.29324239 |
| mean anomaly at epoch: | 315.8463° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|