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 22267.56208428 .00000150 00000-0 13677-3 0 9990
2 27437 82.9464 80.6871 0044609 37.3273 323.0969 13.76613811 21211
| Epoch (UTC): | 24 September 2022 13:29:24 |
| Eccentricity: | 0.0044609 |
| inclination: | 82.9464° |
| perigee height: | 943 km |
| apogee height: | 1009 km |
| right ascension of ascending node: | 80.6871° |
| argument of perigee: | 37.3273° |
| revolutions per day: | 13.76613811 |
| mean anomaly at epoch: | 323.0969° |
| orbit number at epoch: | 2121 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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