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 is defined by the following mean orbital elements,
1 37852U 11061C 24128.89144209 .15302630 55204-5 25512-3 0 9997
2 37852 101.6685 304.2226 0010988 294.2865 65.7274 16.47416046687758
| Epoch (UTC): | 07 May 2024 21:23:40 |
| Eccentricity: | 0.0010988 |
| inclination: | 101.6685° |
| perigee height: | 139 km |
| apogee height: | 153 km |
| right ascension of ascending node: | 304.2226° |
| argument of perigee: | 294.2865° |
| revolutions per day: | 16.47416046 |
| mean anomaly at epoch: | 65.7274° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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