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 3214U 68012D 24334.34722685 .00000338 00000-0 64746-3 0 9994
2 3214 89.8429 112.9606 0187044 33.2013 355.8731 13.29061783745988
| Epoch (UTC): | 29 November 2024 08:20:00 |
| Eccentricity: | 0.0187044 |
| inclination: | 89.8429° |
| perigee height: | 1009 km |
| apogee height: | 1291 km |
| right ascension of ascending node: | 112.9606° |
| argument of perigee: | 33.2013° |
| revolutions per day: | 13.29061783 |
| mean anomaly at epoch: | 355.8731° |
| orbit number at epoch: | 74598 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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