View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 57506U 26145.47645330 +.00000000 +00000-0 +19869-4 0 00003
2 57506 43.0046 302.8400 0001794 267.1167 92.9480 15.27568581 00
| Epoch (UTC): | 25 May 2026 11:26:05 |
| Eccentricity: | 0.0001794 |
| inclination: | 43.0046° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 302.8400° |
| argument of perigee: | 267.1167° |
| revolutions per day: | 15.27568581 |
| mean anomaly at epoch: | 92.9480° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|