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 25343.14168772 .00000232 00000-0 89014-4 0 9993
2 27386 98.3594 293.9735 0001144 81.9813 292.3991 14.38997008246156
| Epoch (UTC): | 09 December 2025 03:24:01 |
| Eccentricity: | 0.0001144 |
| inclination: | 98.3594° |
| perigee height: | 761 km |
| apogee height: | 762 km |
| right ascension of ascending node: | 293.9735° |
| argument of perigee: | 81.9813° |
| revolutions per day: | 14.38997008 |
| mean anomaly at epoch: | 292.3991° |
| orbit number at epoch: | 24615 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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