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 23342.89072345 .00000279 00000-0 28713-3 0 9995
2 00082 38.8493 178.2223 1163999 90.2349 283.1462 12.26443769963623
| Epoch (UTC): | 08 December 2023 21:22:38 |
| Eccentricity: | 0.1163999 |
| inclination: | 38.8493° |
| perigee height: | 640 km |
| apogee height: | 2489 km |
| right ascension of ascending node: | 178.2223° |
| argument of perigee: | 90.2349° |
| revolutions per day: | 12.26443769 |
| mean anomaly at epoch: | 283.1462° |
| orbit number at epoch: | 96362 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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