View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 43807U 26052.11489764 +.00000000 +00000-0 +32591-3 0 00003
2 43807 97.4387 109.6995 0005001 358.8446 1.2775 15.18770373 09
| Epoch (UTC): | 21 February 2026 02:45:27 |
| Eccentricity: | 0.0005001 |
| inclination: | 97.4387° |
| perigee height: | 506 km |
| apogee height: | 513 km |
| right ascension of ascending node: | 109.6995° |
| argument of perigee: | 358.8446° |
| revolutions per day: | 15.18770373 |
| mean anomaly at epoch: | 1.2775° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|