View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 00029U 60002B 24280.85370090 .00004948 00000-0 72171-3 0 9993
2 00029 48.3771 79.9808 0022509 129.0181 231.2740 14.76949105450660
| Epoch (UTC): | 06 October 2024 20:29:19 |
| Eccentricity: | 0.0022509 |
| inclination: | 48.3771° |
| perigee height: | 623 km |
| apogee height: | 655 km |
| right ascension of ascending node: | 79.9808° |
| argument of perigee: | 129.0181° |
| revolutions per day: | 14.76949105 |
| mean anomaly at epoch: | 231.2740° |
| orbit number at epoch: | 45066 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|