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 23338.51158491 .00000293 00000-0 10962-3 0 9995
2 27386 98.2559 301.7273 0001316 83.6424 29.2718 14.38460028140445
| Epoch (UTC): | 04 December 2023 12:16:40 |
| Eccentricity: | 0.0001316 |
| inclination: | 98.2559° |
| perigee height: | 762 km |
| apogee height: | 764 km |
| right ascension of ascending node: | 301.7273° |
| argument of perigee: | 83.6424° |
| revolutions per day: | 14.38460028 |
| mean anomaly at epoch: | 29.2718° |
| orbit number at epoch: | 14044 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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