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 23091.56390014 .00000520 00000-0 18464-3 0 9993
2 27386 98.2235 64.7469 0001393 85.5688 29.4705 14.38302732104947
| Epoch (UTC): | 01 April 2023 13:32:00 |
| Eccentricity: | 0.0001393 |
| inclination: | 98.2235° |
| perigee height: | 763 km |
| apogee height: | 765 km |
| right ascension of ascending node: | 64.7469° |
| argument of perigee: | 85.5688° |
| revolutions per day: | 14.38302732 |
| mean anomaly at epoch: | 29.4705° |
| orbit number at epoch: | 10494 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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