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 23851U 96024A 23152.12578849 .00000305 00000-0 24419-3 0 9998
2 23851 98.9292 95.9271 0008845 66.0215 294.1873 13.98170763382909
| Epoch (UTC): | 01 June 2023 03:01:08 |
| Eccentricity: | 0.0008845 |
| inclination: | 98.9292° |
| perigee height: | 894 km |
| apogee height: | 906 km |
| right ascension of ascending node: | 95.9271° |
| argument of perigee: | 66.0215° |
| revolutions per day: | 13.98170763 |
| mean anomaly at epoch: | 294.1873° |
| orbit number at epoch: | 38290 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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