View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 65921U 26145.36161407 +.00000000 +00000-0 +35529-3 0 00009
2 65921 53.1568 169.7783 0000764 59.6691 300.4386 15.30204500 01
| Epoch (UTC): | 25 May 2026 08:40:43 |
| Eccentricity: | 0.0000764 |
| inclination: | 53.1568° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 169.7783° |
| argument of perigee: | 59.6691° |
| revolutions per day: | 15.30204500 |
| mean anomaly at epoch: | 300.4386° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|