View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 37224U 26073.95689728 +.00000000 +00000-0 +27150-3 0 00001
2 37224 71.9705 293.7197 0016718 247.8216 112.1181 14.93310617 00
| Epoch (UTC): | 14 March 2026 22:57:55 |
| Eccentricity: | 0.0016718 |
| inclination: | 71.9705° |
| perigee height: | 576 km |
| apogee height: | 599 km |
| right ascension of ascending node: | 293.7197° |
| argument of perigee: | 247.8216° |
| revolutions per day: | 14.93310617 |
| mean anomaly at epoch: | 112.1181° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|