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 23332.83804986 .00000728 00000-0 40485-3 0 9998
2 00012 32.9073 261.2914 1660161 222.2470 123.7763 11.45880086424329
| Epoch (UTC): | 28 November 2023 20:06:47 |
| Eccentricity: | 0.1660161 |
| inclination: | 32.9073° |
| perigee height: | 553 km |
| apogee height: | 3312 km |
| right ascension of ascending node: | 261.2914° |
| argument of perigee: | 222.2470° |
| revolutions per day: | 11.45880086 |
| mean anomaly at epoch: | 123.7763° |
| orbit number at epoch: | 42432 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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