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 23093U 94024B 23156.88039987 .00000036 00000-0 20581-4 0 9994
2 23093 82.9449 292.9233 0010486 22.2991 337.8621 13.77976799931344
| Epoch (UTC): | 05 June 2023 21:07:46 |
| Eccentricity: | 0.0010486 |
| inclination: | 82.9449° |
| perigee height: | 963 km |
| apogee height: | 979 km |
| right ascension of ascending node: | 292.9233° |
| argument of perigee: | 22.2991° |
| revolutions per day: | 13.77976799 |
| mean anomaly at epoch: | 337.8621° |
| orbit number at epoch: | 93134 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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