View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 23463U 26159.11817529 +.00000000 +00000-0 +54997-4 0 00006
2 23463 82.9282 22.6279 0039264 162.8054 310.4283 13.72734393 02
| Epoch (UTC): | 08 June 2026 02:50:10 |
| Eccentricity: | 0.0039264 |
| inclination: | 82.9282° |
| perigee height: | 961 km |
| apogee height: | 1019 km |
| right ascension of ascending node: | 22.6279° |
| argument of perigee: | 162.8054° |
| revolutions per day: | 13.72734393 |
| mean anomaly at epoch: | 310.4283° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|