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 39439U 13066Z 23331.80637335 .00013456 00000-0 12501-2 0 9991
2 39439 97.7010 293.2516 0054971 92.8487 267.9026 14.93330614541709
| Epoch (UTC): | 27 November 2023 19:21:10 |
| Eccentricity: | 0.0054971 |
| inclination: | 97.7010° |
| perigee height: | 549 km |
| apogee height: | 626 km |
| right ascension of ascending node: | 293.2516° |
| argument of perigee: | 92.8487° |
| revolutions per day: | 14.93330614 |
| mean anomaly at epoch: | 267.9026° |
| orbit number at epoch: | 54170 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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