View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 57644U 26145.02194471 +.00000000 +00000-0 +14436-3 0 00006
2 57644 43.0046 21.1951 0001407 272.3301 87.7390 15.27577006 08
| Epoch (UTC): | 25 May 2026 00:31:36 |
| Eccentricity: | 0.0001407 |
| inclination: | 43.0046° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 21.1951° |
| argument of perigee: | 272.3301° |
| revolutions per day: | 15.27577006 |
| mean anomaly at epoch: | 87.7390° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|