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 16012U 85079B 24278.48924000 .00001358 00000-0 46424-3 0 9999
2 16012 74.0568 283.4853 0016000 243.4532 116.4981 14.37208476 46366
| Epoch (UTC): | 04 October 2024 11:44:30 |
| Eccentricity: | 0.0016000 |
| inclination: | 74.0568° |
| perigee height: | 756 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 283.4853° |
| argument of perigee: | 243.4532° |
| revolutions per day: | 14.37208476 |
| mean anomaly at epoch: | 116.4981° |
| orbit number at epoch: | 4636 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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