View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 27006U 26017.91308257 +.00000000 +00000-0 +26769-4 0 00003
2 27006 99.7590 182.9830 0015186 116.5150 48.0572 13.71088864 09
| Epoch (UTC): | 17 January 2026 21:54:50 |
| Eccentricity: | 0.0015186 |
| inclination: | 99.7590° |
| perigee height: | 984 km |
| apogee height: | 1007 km |
| right ascension of ascending node: | 182.9830° |
| argument of perigee: | 116.5150° |
| revolutions per day: | 13.71088864 |
| mean anomaly at epoch: | 48.0572° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|