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 23151.94456708 .00000167 00000-0 16439-3 0 9993
2 15752 82.9478 142.3050 0023504 198.6238 161.4059 13.73189949904065
| Epoch (UTC): | 31 May 2023 22:40:10 |
| Eccentricity: | 0.0023504 |
| inclination: | 82.9478° |
| perigee height: | 971 km |
| apogee height: | 1005 km |
| right ascension of ascending node: | 142.3050° |
| argument of perigee: | 198.6238° |
| revolutions per day: | 13.73189949 |
| mean anomaly at epoch: | 161.4059° |
| orbit number at epoch: | 90406 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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