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 25316.86042883 .00000341 00000-0 12424-3 0 9997
2 27386 98.3552 268.3660 0001298 82.6107 304.1440 14.38982663242379
| Epoch (UTC): | 12 November 2025 20:39:01 |
| Eccentricity: | 0.0001298 |
| inclination: | 98.3552° |
| perigee height: | 761 km |
| apogee height: | 763 km |
| right ascension of ascending node: | 268.3660° |
| argument of perigee: | 82.6107° |
| revolutions per day: | 14.38982663 |
| mean anomaly at epoch: | 304.1440° |
| orbit number at epoch: | 24237 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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