View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 57004U 26145.60240213 +.00000000 +00000-0 +41696-3 0 00004
2 57004 97.4934 255.4090 0008439 109.9652 250.2498 15.29916851 02
| Epoch (UTC): | 25 May 2026 14:27:27 |
| Eccentricity: | 0.0008439 |
| inclination: | 97.4934° |
| perigee height: | 470 km |
| apogee height: | 482 km |
| right ascension of ascending node: | 255.4090° |
| argument of perigee: | 109.9652° |
| revolutions per day: | 15.29916851 |
| mean anomaly at epoch: | 250.2498° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|