View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 65119U 26145.60547446 +.00000000 +00000-0 +20275-3 0 00008
2 65119 49.9889 279.1813 0010161 322.2662 37.7563 14.83887180 03
| Epoch (UTC): | 25 May 2026 14:31:52 |
| Eccentricity: | 0.0010161 |
| inclination: | 49.9889° |
| perigee height: | 610 km |
| apogee height: | 624 km |
| right ascension of ascending node: | 279.1813° |
| argument of perigee: | 322.2662° |
| revolutions per day: | 14.83887180 |
| mean anomaly at epoch: | 37.7563° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|