View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 24842U 26088.06978198 +.00000000 +00000-0 +16016-3 0 00002
2 24842 86.4394 84.0415 0012506 220.6286 139.3986 14.48038537 00
| Epoch (UTC): | 29 March 2026 01:40:29 |
| Eccentricity: | 0.0012506 |
| inclination: | 86.4394° |
| perigee height: | 723 km |
| apogee height: | 741 km |
| right ascension of ascending node: | 84.0415° |
| argument of perigee: | 220.6286° |
| revolutions per day: | 14.48038537 |
| mean anomaly at epoch: | 139.3986° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|