View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 23827U 26150.03474352 +.00000000 +00000-0 +83479-4 0 00002
2 23827 99.0289 173.0442 0003335 11.3043 348.8209 14.23729160 07
| Epoch (UTC): | 30 May 2026 00:50:01 |
| Eccentricity: | 0.0003335 |
| inclination: | 99.0289° |
| perigee height: | 810 km |
| apogee height: | 815 km |
| right ascension of ascending node: | 173.0442° |
| argument of perigee: | 11.3043° |
| revolutions per day: | 14.23729160 |
| mean anomaly at epoch: | 348.8209° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|