View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 58713U 26145.54452234 +.00000000 +00000-0 +28513-4 0 00007
2 58713 53.1606 232.8456 0000913 87.7741 272.3365 15.30194505 05
| Epoch (UTC): | 25 May 2026 13:04:06 |
| Eccentricity: | 0.0000913 |
| inclination: | 53.1606° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 232.8456° |
| argument of perigee: | 87.7741° |
| revolutions per day: | 15.30194505 |
| mean anomaly at epoch: | 272.3365° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|