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 32258U 07046A 23274.14273872 .00000030 00000-0 00000+0 0 9991
2 32258 0.0202 184.6651 0000922 25.5777 216.7449 1.00269443 58390
| Epoch (UTC): | 01 October 2023 03:25:32 |
| Eccentricity: | 0.0000922 |
| inclination: | 0.0202° |
| perigee height: | 35783 km |
| apogee height: | 35791 km |
| right ascension of ascending node: | 184.6651° |
| argument of perigee: | 25.5777° |
| revolutions per day: | 1.00269443 |
| mean anomaly at epoch: | 216.7449° |
| orbit number at epoch: | 5839 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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