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 27386U 02009A 23030.48161733 .00000250 00000-0 95765-4 0 9991
2 27386 98.2128 6.2848 0001190 88.2036 21.4864 14.38231563 96099
| Epoch (UTC): | 30 January 2023 11:33:31 |
| Eccentricity: | 0.0001190 |
| inclination: | 98.2128° |
| perigee height: | 763 km |
| apogee height: | 765 km |
| right ascension of ascending node: | 6.2848° |
| argument of perigee: | 88.2036° |
| revolutions per day: | 14.38231563 |
| mean anomaly at epoch: | 21.4864° |
| orbit number at epoch: | 9609 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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