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 17369U 87011A 23340.28870355 .00000045 00000-0 54462-4 0 9997
2 17369 65.0115 315.7645 0019593 283.2946 76.5953 14.31603172976519
| Epoch (UTC): | 06 December 2023 06:55:43 |
| Eccentricity: | 0.0019593 |
| inclination: | 65.0115° |
| perigee height: | 772 km |
| apogee height: | 800 km |
| right ascension of ascending node: | 315.7645° |
| argument of perigee: | 283.2946° |
| revolutions per day: | 14.31603172 |
| mean anomaly at epoch: | 76.5953° |
| orbit number at epoch: | 97651 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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