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 24251.56015770 .00003259 00000-0 71446-3 0 9993
2 00047 66.6685 345.6164 0230441 254.0180 103.5431 14.43815110357250
| Epoch (UTC): | 07 September 2024 13:26:37 |
| Eccentricity: | 0.0230441 |
| inclination: | 66.6685° |
| perigee height: | 582 km |
| apogee height: | 910 km |
| right ascension of ascending node: | 345.6164° |
| argument of perigee: | 254.0180° |
| revolutions per day: | 14.43815110 |
| mean anomaly at epoch: | 103.5431° |
| orbit number at epoch: | 35725 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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