View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 43831U 26145.63603258 +.00000000 +00000-0 +18875-3 0 00005
2 43831 97.3081 207.6542 0009008 204.3622 155.7193 15.27776325 07
| Epoch (UTC): | 25 May 2026 15:15:53 |
| Eccentricity: | 0.0009008 |
| inclination: | 97.3081° |
| perigee height: | 476 km |
| apogee height: | 489 km |
| right ascension of ascending node: | 207.6542° |
| argument of perigee: | 204.3622° |
| revolutions per day: | 15.27776325 |
| mean anomaly at epoch: | 155.7193° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|