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 24262.83379279 .00010591 00000-0 96623-3 0 9999
2 39444 97.7284 220.2358 0045811 185.6082 174.4631 14.94462353584086
| Epoch (UTC): | 18 September 2024 20:00:39 |
| Eccentricity: | 0.0045811 |
| inclination: | 97.7284° |
| perigee height: | 552 km |
| apogee height: | 616 km |
| right ascension of ascending node: | 220.2358° |
| argument of perigee: | 185.6082° |
| revolutions per day: | 14.94462353 |
| mean anomaly at epoch: | 174.4631° |
| orbit number at epoch: | 58408 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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