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 23341.90264163 .00000149 00000-0 62333-4 0 9996
2 27386 98.2562 304.9887 0001286 82.9554 300.2128 14.38461557140936
| Epoch (UTC): | 07 December 2023 21:39:48 |
| Eccentricity: | 0.0001286 |
| inclination: | 98.2562° |
| perigee height: | 762 km |
| apogee height: | 764 km |
| right ascension of ascending node: | 304.9887° |
| argument of perigee: | 82.9554° |
| revolutions per day: | 14.38461557 |
| mean anomaly at epoch: | 300.2128° |
| orbit number at epoch: | 14093 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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