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 23336.50044038 .00001146 00000-0 28027-3 0 9999
2 00047 66.6668 16.1164 0217169 99.1530 263.4212 14.43186230316836
| Epoch (UTC): | 02 December 2023 12:00:38 |
| Eccentricity: | 0.0217169 |
| inclination: | 66.6668° |
| perigee height: | 593 km |
| apogee height: | 903 km |
| right ascension of ascending node: | 16.1164° |
| argument of perigee: | 99.1530° |
| revolutions per day: | 14.43186230 |
| mean anomaly at epoch: | 263.4212° |
| orbit number at epoch: | 31683 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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