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 25343.84051390 .00000274 00000-0 10275-3 0 9995
2 27386 98.3595 294.6546 0001138 82.2120 310.2641 14.38997695246258
| Epoch (UTC): | 09 December 2025 20:10:20 |
| Eccentricity: | 0.0001138 |
| inclination: | 98.3595° |
| perigee height: | 761 km |
| apogee height: | 762 km |
| right ascension of ascending node: | 294.6546° |
| argument of perigee: | 82.2120° |
| revolutions per day: | 14.38997695 |
| mean anomaly at epoch: | 310.2641° |
| orbit number at epoch: | 24625 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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