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 23036.94280953 .00000266 00000-0 10114-3 0 9995
2 27386 98.2142 12.4647 0001229 89.9621 334.0200 14.38235757 97022
| Epoch (UTC): | 05 February 2023 22:37:38 |
| Eccentricity: | 0.0001229 |
| inclination: | 98.2142° |
| perigee height: | 763 km |
| apogee height: | 765 km |
| right ascension of ascending node: | 12.4647° |
| argument of perigee: | 89.9621° |
| revolutions per day: | 14.38235757 |
| mean anomaly at epoch: | 334.0200° |
| orbit number at epoch: | 9702 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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