View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 15752U 26037.73766885 +.00000000 +00000-0 +92195-4 0 00001
2 15752 82.9527 137.9148 0023573 353.9539 6.1328 13.73342403 05
| Epoch (UTC): | 06 February 2026 17:42:14 |
| Eccentricity: | 0.0023573 |
| inclination: | 82.9527° |
| perigee height: | 970 km |
| apogee height: | 1005 km |
| right ascension of ascending node: | 137.9148° |
| argument of perigee: | 353.9539° |
| revolutions per day: | 13.73342403 |
| mean anomaly at epoch: | 6.1328° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|