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 27437U 02026B 23029.90174485 .00000130 00000-0 11572-3 0 9990
2 27437 82.9526 346.1890 0044853 40.9470 319.5041 13.76639950 38739
| Epoch (UTC): | 29 January 2023 21:38:30 |
| Eccentricity: | 0.0044853 |
| inclination: | 82.9526° |
| perigee height: | 943 km |
| apogee height: | 1009 km |
| right ascension of ascending node: | 346.1890° |
| argument of perigee: | 40.9470° |
| revolutions per day: | 13.76639950 |
| mean anomaly at epoch: | 319.5041° |
| orbit number at epoch: | 3873 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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