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 25348.84467566 .00000167 00000-0 68088-4 0 9993
2 27386 98.3602 299.5319 0001135 83.7193 297.2822 14.39000147246974
| Epoch (UTC): | 14 December 2025 20:16:19 |
| Eccentricity: | 0.0001135 |
| inclination: | 98.3602° |
| perigee height: | 761 km |
| apogee height: | 762 km |
| right ascension of ascending node: | 299.5319° |
| argument of perigee: | 83.7193° |
| revolutions per day: | 14.39000147 |
| mean anomaly at epoch: | 297.2822° |
| orbit number at epoch: | 24697 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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