View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 57038U 26145.62481251 +.00000000 +00000-0 +44075-3 0 00006
2 57038 97.4922 257.6742 0007806 151.6735 208.4933 15.34166269 02
| Epoch (UTC): | 25 May 2026 14:59:43 |
| Eccentricity: | 0.0007806 |
| inclination: | 97.4922° |
| perigee height: | 458 km |
| apogee height: | 469 km |
| right ascension of ascending node: | 257.6742° |
| argument of perigee: | 151.6735° |
| revolutions per day: | 15.34166269 |
| mean anomaly at epoch: | 208.4933° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|