View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 39090U 26071.48861705 +.00000000 +00000-0 +16853-3 0 00005
2 39090 98.3891 254.1108 0009185 153.7514 206.4140 14.37097776 09
| Epoch (UTC): | 12 March 2026 11:43:36 |
| Eccentricity: | 0.0009185 |
| inclination: | 98.3891° |
| perigee height: | 762 km |
| apogee height: | 775 km |
| right ascension of ascending node: | 254.1108° |
| argument of perigee: | 153.7514° |
| revolutions per day: | 14.37097776 |
| mean anomaly at epoch: | 206.4140° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|