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 23268.25109850 .00000867 00000-0 48685-3 0 9994
2 00012 32.9079 127.8693 1660020 241.7900 100.5358 11.45796084416917
| Epoch (UTC): | 25 September 2023 06:01:34 |
| Eccentricity: | 0.1660020 |
| inclination: | 32.9079° |
| perigee height: | 553 km |
| apogee height: | 3313 km |
| right ascension of ascending node: | 127.8693° |
| argument of perigee: | 241.7900° |
| revolutions per day: | 11.45796084 |
| mean anomaly at epoch: | 100.5358° |
| orbit number at epoch: | 41691 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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