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 15752U 85041B 23331.62625544 .00000082 00000-0 71918-4 0 9994
2 15752 82.9514 9.7360 0025306 63.9754 296.4003 13.73208938928722
| Epoch (UTC): | 27 November 2023 15:01:48 |
| Eccentricity: | 0.0025306 |
| inclination: | 82.9514° |
| perigee height: | 969 km |
| apogee height: | 1007 km |
| right ascension of ascending node: | 9.7360° |
| argument of perigee: | 63.9754° |
| revolutions per day: | 13.73208938 |
| mean anomaly at epoch: | 296.4003° |
| orbit number at epoch: | 92872 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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