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 37852U 11061C 23270.65444738 .00047520 00000-0 11459-2 0 9999
2 37852 101.7098 299.9843 0093530 70.2166 290.9118 15.36582851653030
| Epoch (UTC): | 27 September 2023 15:42:24 |
| Eccentricity: | 0.0093530 |
| inclination: | 101.7098° |
| perigee height: | 392 km |
| apogee height: | 520 km |
| right ascension of ascending node: | 299.9843° |
| argument of perigee: | 70.2166° |
| revolutions per day: | 15.36582851 |
| mean anomaly at epoch: | 290.9118° |
| orbit number at epoch: | 65303 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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