View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 23751U 26100.04587352 +.00000000 +00000-0 +63694-4 0 00006
2 23751 99.0265 117.3715 0001087 100.0349 260.0951 14.23552485 01
| Epoch (UTC): | 10 April 2026 01:06:03 |
| Eccentricity: | 0.0001087 |
| inclination: | 99.0265° |
| perigee height: | 813 km |
| apogee height: | 814 km |
| right ascension of ascending node: | 117.3715° |
| argument of perigee: | 100.0349° |
| revolutions per day: | 14.23552485 |
| mean anomaly at epoch: | 260.0951° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|