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 37423U 99025EGR 23331.97250654 .00002086 00000-0 13242-2 0 9994
2 37423 98.8575 30.5698 0051035 93.5491 267.1515 14.04266583531307
| Epoch (UTC): | 27 November 2023 23:20:24 |
| Eccentricity: | 0.0051035 |
| inclination: | 98.8575° |
| perigee height: | 842 km |
| apogee height: | 916 km |
| right ascension of ascending node: | 30.5698° |
| argument of perigee: | 93.5491° |
| revolutions per day: | 14.04266583 |
| mean anomaly at epoch: | 267.1515° |
| orbit number at epoch: | 53130 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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