View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 39426U 26088.19947002 +.00000000 +00000-0 +26427-3 0 00007
2 39426 97.8428 2.4853 0091605 111.1323 249.9709 14.78063632 09
| Epoch (UTC): | 29 March 2026 04:47:14 |
| Eccentricity: | 0.0091605 |
| inclination: | 97.8428° |
| perigee height: | 571 km |
| apogee height: | 700 km |
| right ascension of ascending node: | 2.4853° |
| argument of perigee: | 111.1323° |
| revolutions per day: | 14.78063632 |
| mean anomaly at epoch: | 249.9709° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|