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 23335.74340363 .00064581 00000-0 14465-2 0 9999
2 37855 101.6964 33.7173 0094039 243.1754 115.9835 15.38594552662689
| Epoch (UTC): | 01 December 2023 17:50:30 |
| Eccentricity: | 0.0094039 |
| inclination: | 101.6964° |
| perigee height: | 386 km |
| apogee height: | 514 km |
| right ascension of ascending node: | 33.7173° |
| argument of perigee: | 243.1754° |
| revolutions per day: | 15.38594552 |
| mean anomaly at epoch: | 115.9835° |
| orbit number at epoch: | 66268 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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