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 43666U 18083E 23266.09204701 .00059530 00000-0 12257-2 0 9998
2 43666 97.3723 298.7174 0010067 123.2889 236.9325 15.45682339272280
| Epoch (UTC): | 23 September 2023 02:12:32 |
| Eccentricity: | 0.0010067 |
| inclination: | 97.3723° |
| perigee height: | 422 km |
| apogee height: | 436 km |
| right ascension of ascending node: | 298.7174° |
| argument of perigee: | 123.2889° |
| revolutions per day: | 15.45682339 |
| mean anomaly at epoch: | 236.9325° |
| orbit number at epoch: | 27228 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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