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 12U 59001B 23337.10778508 .00000706 00000-0 39037-3 0 9990
2 12 32.9095 246.3145 1660379 244.7448 97.2217 11.45886714667397
| Epoch (UTC): | 03 December 2023 02:35:12 |
| Eccentricity: | 0.1660379 |
| inclination: | 32.9095° |
| perigee height: | 553 km |
| apogee height: | 3312 km |
| right ascension of ascending node: | 246.3145° |
| argument of perigee: | 244.7448° |
| revolutions per day: | 11.45886714 |
| mean anomaly at epoch: | 97.2217° |
| orbit number at epoch: | 66739 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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