View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 27848U 26038.98216427 +.00000000 +00000-0 +17488-3 0 00001
2 27848 98.6805 48.9686 0008841 213.5570 146.5049 14.23539500 03
| Epoch (UTC): | 07 February 2026 23:34:18 |
| Eccentricity: | 0.0008841 |
| inclination: | 98.6805° |
| perigee height: | 807 km |
| apogee height: | 820 km |
| right ascension of ascending node: | 48.9686° |
| argument of perigee: | 213.5570° |
| revolutions per day: | 14.23539500 |
| mean anomaly at epoch: | 146.5049° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|