View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 40967U 26101.46996772 +.00000000 +00000-0 +17314-3 0 00008
2 40967 64.7740 126.2537 0128350 82.7778 278.7904 14.90573784 05
| Epoch (UTC): | 11 April 2026 11:16:45 |
| Eccentricity: | 0.0128350 |
| inclination: | 64.7740° |
| perigee height: | 507 km |
| apogee height: | 686 km |
| right ascension of ascending node: | 126.2537° |
| argument of perigee: | 82.7778° |
| revolutions per day: | 14.90573784 |
| mean anomaly at epoch: | 278.7904° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|