View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 64303U 26145.33654616 +.00000000 +00000-0 +26940-3 0 00005
2 64303 70.0019 1.0373 0002425 269.1431 90.9450 14.98335976 00
| Epoch (UTC): | 25 May 2026 08:04:37 |
| Eccentricity: | 0.0002425 |
| inclination: | 70.0019° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 1.0373° |
| argument of perigee: | 269.1431° |
| revolutions per day: | 14.98335976 |
| mean anomaly at epoch: | 90.9450° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|