View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 65039U 26145.58335647 +.00000000 +00000-0 -24670-3 0 00008
2 65039 53.1595 296.7061 0001276 85.9034 43.1413 15.30217043 01
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001276 |
| inclination: | 53.1595° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 296.7061° |
| argument of perigee: | 85.9034° |
| revolutions per day: | 15.30217043 |
| mean anomaly at epoch: | 43.1413° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|