View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 08709U 26053.27123412 +.00000000 +00000-0 +26365-4 0 00001
2 08709 69.6755 15.6705 0007748 62.3143 43.1385 13.71734432 02
| Epoch (UTC): | 22 February 2026 06:30:34 |
| Eccentricity: | 0.0007748 |
| inclination: | 69.6755° |
| perigee height: | 988 km |
| apogee height: | 999 km |
| right ascension of ascending node: | 15.6705° |
| argument of perigee: | 62.3143° |
| revolutions per day: | 13.71734432 |
| mean anomaly at epoch: | 43.1385° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|