View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 40053U 26118.52625557 +.00000000 +00000-0 +14469-3 0 00007
2 40053 98.0663 182.2909 0001528 78.0826 282.0546 14.60914309 08
| Epoch (UTC): | 28 April 2026 12:37:48 |
| Eccentricity: | 0.0001528 |
| inclination: | 98.0663° |
| perigee height: | 689 km |
| apogee height: | 691 km |
| right ascension of ascending node: | 182.2909° |
| argument of perigee: | 78.0826° |
| revolutions per day: | 14.60914309 |
| mean anomaly at epoch: | 282.0546° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|