View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 37224U 26066.38701829 +.00000000 +00000-0 +32903-3 0 00009
2 37224 71.9714 310.8551 0016909 260.5654 99.3604 14.93266454 00
| Epoch (UTC): | 07 March 2026 09:17:18 |
| Eccentricity: | 0.0016909 |
| inclination: | 71.9714° |
| perigee height: | 576 km |
| apogee height: | 600 km |
| right ascension of ascending node: | 310.8551° |
| argument of perigee: | 260.5654° |
| revolutions per day: | 14.93266454 |
| mean anomaly at epoch: | 99.3604° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|