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 32290U 07055B 23265.93086140 .00124754 00000-0 70352-3 0 9995
2 32290 97.6057 145.9056 0023338 175.8284 184.3182 15.78417475884394
| Epoch (UTC): | 22 September 2023 22:20:26 |
| Eccentricity: | 0.0023338 |
| inclination: | 97.6057° |
| perigee height: | 319 km |
| apogee height: | 350 km |
| right ascension of ascending node: | 145.9056° |
| argument of perigee: | 175.8284° |
| revolutions per day: | 15.78417475 |
| mean anomaly at epoch: | 184.3182° |
| orbit number at epoch: | 88439 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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