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 23271.91166224 .00000741 00000-0 41270-3 0 9993
2 00012 32.9095 115.0317 1660200 261.0774 79.9055 11.45800942417330
| Epoch (UTC): | 28 September 2023 21:52:47 |
| Eccentricity: | 0.1660200 |
| inclination: | 32.9095° |
| perigee height: | 553 km |
| apogee height: | 3313 km |
| right ascension of ascending node: | 115.0317° |
| argument of perigee: | 261.0774° |
| revolutions per day: | 11.45800942 |
| mean anomaly at epoch: | 79.9055° |
| orbit number at epoch: | 41733 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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