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 23334.11751274 .00060771 00000-0 13690-2 0 9992
2 37855 101.6966 31.1329 0094479 248.2420 110.8733 15.38405131662438
| Epoch (UTC): | 30 November 2023 02:49:13 |
| Eccentricity: | 0.0094479 |
| inclination: | 101.6966° |
| perigee height: | 386 km |
| apogee height: | 515 km |
| right ascension of ascending node: | 31.1329° |
| argument of perigee: | 248.2420° |
| revolutions per day: | 15.38405131 |
| mean anomaly at epoch: | 110.8733° |
| orbit number at epoch: | 66243 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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