View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 27607U 02058C 23331.74985315 .00003446 00000-0 48599-3 0 9996
2 27607 64.5541 123.2623 0050059 187.9466 172.0851 14.77969373126603
| Epoch (UTC): | 27 November 2023 17:59:47 |
| Eccentricity: | 0.0050059 |
| inclination: | 64.5541° |
| perigee height: | 600 km |
| apogee height: | 671 km |
| right ascension of ascending node: | 123.2623° |
| argument of perigee: | 187.9466° |
| revolutions per day: | 14.77969373 |
| mean anomaly at epoch: | 172.0851° |
| orbit number at epoch: | 12660 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|