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 23334.70285678 .00060008 00000-0 13501-2 0 9991
2 37855 101.6965 32.0632 0094275 246.5359 112.5939 15.38464565662523
| Epoch (UTC): | 30 November 2023 16:52:06 |
| Eccentricity: | 0.0094275 |
| inclination: | 101.6965° |
| perigee height: | 386 km |
| apogee height: | 515 km |
| right ascension of ascending node: | 32.0632° |
| argument of perigee: | 246.5359° |
| revolutions per day: | 15.38464565 |
| mean anomaly at epoch: | 112.5939° |
| orbit number at epoch: | 66252 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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