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 23248.97808300 0.00000000 00000-0 00000-0 0 01
2 23223 12.7604 17.2367 0030291 97.2168 263.1461 1.00270000 01
| Epoch (UTC): | 05 September 2023 23:28:26 |
| Eccentricity: | 0.0030291 |
| inclination: | 12.7604° |
| perigee height: | 35659 km |
| apogee height: | 35914 km |
| right ascension of ascending node: | 17.2367° |
| argument of perigee: | 97.2168° |
| revolutions per day: | 1.00270000 |
| mean anomaly at epoch: | 263.1461° |
| 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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