View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 43643U 26145.62432162 +.00000000 +00000-0 +11818-3 0 00009
2 43643 98.1495 174.3941 0004504 298.0286 62.0460 14.63139493 06
| Epoch (UTC): | 25 May 2026 14:59:01 |
| Eccentricity: | 0.0004504 |
| inclination: | 98.1495° |
| perigee height: | 680 km |
| apogee height: | 686 km |
| right ascension of ascending node: | 174.3941° |
| argument of perigee: | 298.0286° |
| revolutions per day: | 14.63139493 |
| mean anomaly at epoch: | 62.0460° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|