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 26374U 00030A 23331.77632171 .00014002 00000-0 10247-2 0 9994
2 26374 68.9268 96.0761 0567120 99.4140 267.1519 14.24941497188047
| Epoch (UTC): | 27 November 2023 18:37:54 |
| Eccentricity: | 0.0567120 |
| inclination: | 68.9268° |
| perigee height: | 401 km |
| apogee height: | 1216 km |
| right ascension of ascending node: | 96.0761° |
| argument of perigee: | 99.4140° |
| revolutions per day: | 14.24941497 |
| mean anomaly at epoch: | 267.1519° |
| orbit number at epoch: | 18804 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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