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 24280.64121855 .00023127 00000-0 20661-2 0 9990
2 39444 97.7327 237.7805 0047920 127.5005 233.0587 14.95019797587331
| Epoch (UTC): | 06 October 2024 15:23:21 |
| Eccentricity: | 0.0047920 |
| inclination: | 97.7327° |
| perigee height: | 549 km |
| apogee height: | 615 km |
| right ascension of ascending node: | 237.7805° |
| argument of perigee: | 127.5005° |
| revolutions per day: | 14.95019797 |
| mean anomaly at epoch: | 233.0587° |
| orbit number at epoch: | 58733 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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