View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 43807U 26103.16054014 +.00000000 +00000-0 +22100-3 0 00006
2 43807 97.4290 159.9410 0006550 152.1011 208.0577 15.19660406 08
| Epoch (UTC): | 13 April 2026 03:51:10 |
| Eccentricity: | 0.0006550 |
| inclination: | 97.4290° |
| perigee height: | 502 km |
| apogee height: | 511 km |
| right ascension of ascending node: | 159.9410° |
| argument of perigee: | 152.1011° |
| revolutions per day: | 15.19660406 |
| mean anomaly at epoch: | 208.0577° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|