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 00012U 59001B 23263.89398322 .00000756 00000-0 42387-3 0 9993
2 00012 32.9050 143.1513 1659752 218.8274 128.0751 11.45788524416414
| Epoch (UTC): | 20 September 2023 21:27:20 |
| Eccentricity: | 0.1659752 |
| inclination: | 32.9050° |
| perigee height: | 553 km |
| apogee height: | 3312 km |
| right ascension of ascending node: | 143.1513° |
| argument of perigee: | 218.8274° |
| revolutions per day: | 11.45788524 |
| mean anomaly at epoch: | 128.0751° |
| orbit number at epoch: | 41641 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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