View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 29528U 26020.95272193 +.00000000 +00000-0 +28953-3 0 00007
2 29528 51.3064 305.1276 6002289 88.1112 358.1877 3.64298943 06
| Epoch (UTC): | 20 January 2026 22:51:55 |
| Eccentricity: | 0.6002289 |
| inclination: | 51.3064° |
| perigee height: | 754 km |
| apogee height: | 22172 km |
| right ascension of ascending node: | 305.1276° |
| argument of perigee: | 88.1112° |
| revolutions per day: | 3.64298943 |
| mean anomaly at epoch: | 358.1877° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|