View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 65746U 26145.25306505 +.00000000 +00000-0 +86734-3 0 00006
2 65746 53.1621 337.4132 0000236 51.4135 308.6886 15.30221352 04
| Epoch (UTC): | 25 May 2026 06:04:24 |
| Eccentricity: | 0.0000236 |
| inclination: | 53.1621° |
| perigee height: | 475 km |
| apogee height: | 475 km |
| right ascension of ascending node: | 337.4132° |
| argument of perigee: | 51.4135° |
| revolutions per day: | 15.30221352 |
| mean anomaly at epoch: | 308.6886° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|