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 23092.17017931 .00000534 00000-0 18902-3 0 9997
2 27386 98.2237 65.3276 0001387 85.3977 287.0649 14.38303486105031
| Epoch (UTC): | 02 April 2023 04:05:03 |
| Eccentricity: | 0.0001387 |
| inclination: | 98.2237° |
| perigee height: | 763 km |
| apogee height: | 765 km |
| right ascension of ascending node: | 65.3276° |
| argument of perigee: | 85.3977° |
| revolutions per day: | 14.38303486 |
| mean anomaly at epoch: | 287.0649° |
| orbit number at epoch: | 10503 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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