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 23223U 94054A 24213.07012549 0.00000000 00000-0 00000-0 0 07
2 23223 12.9554 15.1853 0033666 87.3252 273.0792 1.00270000 04
| Epoch (UTC): | 31 July 2024 01:40:58 |
| Eccentricity: | 0.0033666 |
| inclination: | 12.9554° |
| perigee height: | 35645 km |
| apogee height: | 35928 km |
| right ascension of ascending node: | 15.1853° |
| argument of perigee: | 87.3252° |
| revolutions per day: | 1.00270000 |
| mean anomaly at epoch: | 273.0792° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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