View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 65912U 26145.58335647 +.00000000 +00000-0 +94701-3 0 00009
2 65912 53.1593 168.6699 0001458 78.5685 106.1453 15.33537475 06
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001458 |
| inclination: | 53.1593° |
| perigee height: | 464 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 168.6699° |
| argument of perigee: | 78.5685° |
| revolutions per day: | 15.33537475 |
| mean anomaly at epoch: | 106.1453° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|