View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 57683U 26145.36918154 +.00000000 +00000-0 -24135-4 0 00007
2 57683 53.1596 210.9004 0001149 85.9307 274.1825 15.30185893 05
| Epoch (UTC): | 25 May 2026 08:51:37 |
| Eccentricity: | 0.0001149 |
| inclination: | 53.1596° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 210.9004° |
| argument of perigee: | 85.9307° |
| revolutions per day: | 15.30185893 |
| mean anomaly at epoch: | 274.1825° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|