View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 26930U 26106.67774241 +.00000000 +00000-0 +39160-4 0 00009
2 26930 67.0024 344.2193 0010805 283.2761 76.7136 14.31574558 03
| Epoch (UTC): | 16 April 2026 16:15:56 |
| Eccentricity: | 0.0010805 |
| inclination: | 67.0024° |
| perigee height: | 779 km |
| apogee height: | 794 km |
| right ascension of ascending node: | 344.2193° |
| argument of perigee: | 283.2761° |
| revolutions per day: | 14.31574558 |
| mean anomaly at epoch: | 76.7136° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|