View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 10674U 26106.53686447 +.00000000 +00000-0 +18387-4 0 00000
2 10674 69.3658 15.5735 0163814 172.4468 1.7451 13.43712219 09
| Epoch (UTC): | 16 April 2026 12:53:05 |
| Eccentricity: | 0.0163814 |
| inclination: | 69.3658° |
| perigee height: | 973 km |
| apogee height: | 1218 km |
| right ascension of ascending node: | 15.5735° |
| argument of perigee: | 172.4468° |
| revolutions per day: | 13.43712219 |
| mean anomaly at epoch: | 1.7451° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|