View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 19826U 26106.62740360 +.00000000 +00000-0 +56576-4 0 00005
2 19826 82.9526 328.6910 0031311 62.3411 351.1345 13.72547859 08
| Epoch (UTC): | 16 April 2026 15:03:27 |
| Eccentricity: | 0.0031311 |
| inclination: | 82.9526° |
| perigee height: | 967 km |
| apogee height: | 1014 km |
| right ascension of ascending node: | 328.6910° |
| argument of perigee: | 62.3411° |
| revolutions per day: | 13.72547859 |
| mean anomaly at epoch: | 351.1345° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|