View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 65742U 26145.24040727 +.00000000 +00000-0 +74075-3 0 00007
2 65742 53.1612 337.3372 0001200 89.8613 270.2525 15.30201211 09
| Epoch (UTC): | 25 May 2026 05:46:11 |
| Eccentricity: | 0.0001200 |
| inclination: | 53.1612° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 337.3372° |
| argument of perigee: | 89.8613° |
| revolutions per day: | 15.30201211 |
| mean anomaly at epoch: | 270.2525° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|