View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 49826U 82092KH 23033.53887818 .00085112 00000-0 28428-2 0 9992
2 49826 82.7834 70.5123 0096945 4.5927 355.6177 15.26207661 64584
| Epoch (UTC): | 02 February 2023 12:55:59 |
| Eccentricity: | 0.0096945 |
| inclination: | 82.7834° |
| perigee height: | 420 km |
| apogee height: | 554 km |
| right ascension of ascending node: | 70.5123° |
| argument of perigee: | 4.5927° |
| revolutions per day: | 15.26207661 |
| mean anomaly at epoch: | 355.6177° |
| orbit number at epoch: | 6458 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|