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 39444U 13066AE 23332.45496486 .00008438 00000-0 88498-3 0 9992
2 39444 97.6948 291.4472 0053263 89.8730 270.8590 14.88714303540067
| Epoch (UTC): | 28 November 2023 10:55:08 |
| Eccentricity: | 0.0053263 |
| inclination: | 97.6948° |
| perigee height: | 565 km |
| apogee height: | 639 km |
| right ascension of ascending node: | 291.4472° |
| argument of perigee: | 89.8730° |
| revolutions per day: | 14.88714303 |
| mean anomaly at epoch: | 270.8590° |
| orbit number at epoch: | 54006 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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