View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 27006U 26102.74900904 +.00000000 +00000-0 +25862-4 0 00009
2 27006 99.7736 269.1991 0013758 259.1431 111.8246 13.71093331 08
| Epoch (UTC): | 12 April 2026 17:58:34 |
| Eccentricity: | 0.0013758 |
| inclination: | 99.7736° |
| perigee height: | 986 km |
| apogee height: | 1006 km |
| right ascension of ascending node: | 269.1991° |
| argument of perigee: | 259.1431° |
| revolutions per day: | 13.71093331 |
| mean anomaly at epoch: | 111.8246° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|