View from above orbital plane
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View from above satellite
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Ground track
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The orbit data is extracted from the following two-line orbital elements,
1 00047U 60007C 24277.88194209 .00003480 00000-0 76197-3 0 9995
2 00047 66.6645 275.0246 0229031 235.2753 122.6594 14.43938261361051
| Epoch (UTC): | 03 October 2024 21:09:59 |
| Eccentricity: | 0.0229031 |
| inclination: | 66.6645° |
| perigee height: | 582 km |
| apogee height: | 908 km |
| right ascension of ascending node: | 275.0246° |
| argument of perigee: | 235.2753° |
| revolutions per day: | 14.43938261 |
| mean anomaly at epoch: | 122.6594° |
| orbit number at epoch: | 36105 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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