View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 24836U 26087.93560823 +.00000000 +00000-0 +16209-3 0 00006
2 24836 86.3901 61.9612 0002749 53.3095 306.8357 14.41179177 08
| Epoch (UTC): | 28 March 2026 22:27:16 |
| Eccentricity: | 0.0002749 |
| inclination: | 86.3901° |
| perigee height: | 753 km |
| apogee height: | 757 km |
| right ascension of ascending node: | 61.9612° |
| argument of perigee: | 53.3095° |
| revolutions per day: | 14.41179177 |
| mean anomaly at epoch: | 306.8357° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|