View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 62749U 26145.54712086 +.00000000 +00000-0 +40213-3 0 00005
2 62749 43.0035 83.6327 0001250 262.9886 97.0824 15.27593455 09
| Epoch (UTC): | 25 May 2026 13:07:51 |
| Eccentricity: | 0.0001250 |
| inclination: | 43.0035° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 83.6327° |
| argument of perigee: | 262.9886° |
| revolutions per day: | 15.27593455 |
| mean anomaly at epoch: | 97.0824° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|