View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 00047U 60007C 24254.74659778 .00003121 00000-0 68522-3 0 9997
2 00047 66.6682 337.0723 0230268 251.7532 105.8392 14.43834369357714
| Epoch (UTC): | 10 September 2024 17:55:06 |
| Eccentricity: | 0.0230268 |
| inclination: | 66.6682° |
| perigee height: | 582 km |
| apogee height: | 910 km |
| right ascension of ascending node: | 337.0723° |
| argument of perigee: | 251.7532° |
| revolutions per day: | 14.43834369 |
| mean anomaly at epoch: | 105.8392° |
| orbit number at epoch: | 35771 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|