View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 39090U 26105.88298830 +.00000000 +00000-0 +71586-4 0 00005
2 39090 98.3911 287.6542 0009686 61.7230 298.4933 14.37125770 01
| Epoch (UTC): | 15 April 2026 21:11:30 |
| Eccentricity: | 0.0009686 |
| inclination: | 98.3911° |
| perigee height: | 761 km |
| apogee height: | 775 km |
| right ascension of ascending node: | 287.6542° |
| argument of perigee: | 61.7230° |
| revolutions per day: | 14.37125770 |
| mean anomaly at epoch: | 298.4933° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|