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 23332.95298869 .00000857 00000-0 77577-3 0 9996
2 00082 38.8506 215.0343 1163951 42.2312 326.2352 12.26430948962403
| Epoch (UTC): | 28 November 2023 22:52:18 |
| Eccentricity: | 0.1163951 |
| inclination: | 38.8506° |
| perigee height: | 640 km |
| apogee height: | 2489 km |
| right ascension of ascending node: | 215.0343° |
| argument of perigee: | 42.2312° |
| revolutions per day: | 12.26430948 |
| mean anomaly at epoch: | 326.2352° |
| orbit number at epoch: | 96240 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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