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 00082U 61004B 24280.88816309 .00002116 00000-0 17939-2 0 9991
2 00082 38.8510 135.3480 1165424 114.1385 258.5481 12.27088702 816
| Epoch (UTC): | 06 October 2024 21:18:57 |
| Eccentricity: | 0.1165424 |
| inclination: | 38.8510° |
| perigee height: | 636 km |
| apogee height: | 2487 km |
| right ascension of ascending node: | 135.3480° |
| argument of perigee: | 114.1385° |
| revolutions per day: | 12.27088702 |
| mean anomaly at epoch: | 258.5481° |
| orbit number at epoch: | 81 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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