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 43438U 18039B 24357.82201519 .00012328 00000-0 40413-3 0 9993
2 43438 98.7163 31.3462 0182039 235.9819 122.4006 15.17293167365019
| Epoch (UTC): | 22 December 2024 19:43:42 |
| Eccentricity: | 0.0182039 |
| inclination: | 98.7163° |
| perigee height: | 388 km |
| apogee height: | 639 km |
| right ascension of ascending node: | 31.3462° |
| argument of perigee: | 235.9819° |
| revolutions per day: | 15.17293167 |
| mean anomaly at epoch: | 122.4006° |
| orbit number at epoch: | 36501 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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