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 23334.47677182 .00000399 00000-0 14447-3 0 9998
2 27386 98.2553 297.8470 0001308 84.2147 26.7489 14.38457318139862
| Epoch (UTC): | 30 November 2023 11:26:33 |
| Eccentricity: | 0.0001308 |
| inclination: | 98.2553° |
| perigee height: | 762 km |
| apogee height: | 764 km |
| right ascension of ascending node: | 297.8470° |
| argument of perigee: | 84.2147° |
| revolutions per day: | 14.38457318 |
| mean anomaly at epoch: | 26.7489° |
| orbit number at epoch: | 13986 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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