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 37855U 11061F 23336.71882195 .00045836 00000-0 10258-2 0 9999
2 37855 101.6964 35.2677 0093804 240.1478 119.0404 15.38737551662836
| Epoch (UTC): | 02 December 2023 17:15:06 |
| Eccentricity: | 0.0093804 |
| inclination: | 101.6964° |
| perigee height: | 386 km |
| apogee height: | 514 km |
| right ascension of ascending node: | 35.2677° |
| argument of perigee: | 240.1478° |
| revolutions per day: | 15.38737551 |
| mean anomaly at epoch: | 119.0404° |
| orbit number at epoch: | 66283 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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