View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 37224U 26072.61711139 +.00000000 +00000-0 +26674-3 0 00005
2 37224 71.9708 296.7525 0016748 250.1651 109.7714 14.93303315 05
| Epoch (UTC): | 13 March 2026 14:48:38 |
| Eccentricity: | 0.0016748 |
| inclination: | 71.9708° |
| perigee height: | 576 km |
| apogee height: | 599 km |
| right ascension of ascending node: | 296.7525° |
| argument of perigee: | 250.1651° |
| revolutions per day: | 14.93303315 |
| mean anomaly at epoch: | 109.7714° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|