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 23035.89724240 .00000247 00000-0 94750-4 0 9998
2 27386 98.2139 11.4646 0001226 89.6500 323.9005 14.38235002 96871
| Epoch (UTC): | 04 February 2023 21:32:01 |
| Eccentricity: | 0.0001226 |
| inclination: | 98.2139° |
| perigee height: | 763 km |
| apogee height: | 765 km |
| right ascension of ascending node: | 11.4646° |
| argument of perigee: | 89.6500° |
| revolutions per day: | 14.38235002 |
| mean anomaly at epoch: | 323.9005° |
| orbit number at epoch: | 9687 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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