View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 47823U 26145.35645922 +.00000000 +00000-0 +60869-4 0 00004
2 47823 53.1576 261.4759 0001130 87.7365 272.3765 15.31696709 07
| Epoch (UTC): | 25 May 2026 08:33:18 |
| Eccentricity: | 0.0001130 |
| inclination: | 53.1576° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 261.4759° |
| argument of perigee: | 87.7365° |
| revolutions per day: | 15.31696709 |
| mean anomaly at epoch: | 272.3765° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|