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 25348.38661397 .00000199 00000-0 78310-4 0 9994
2 27386 98.3602 299.0854 0001141 83.6000 85.8332 14.39000077246908
| Epoch (UTC): | 14 December 2025 09:16:43 |
| Eccentricity: | 0.0001141 |
| inclination: | 98.3602° |
| perigee height: | 761 km |
| apogee height: | 762 km |
| right ascension of ascending node: | 299.0854° |
| argument of perigee: | 83.6000° |
| revolutions per day: | 14.39000077 |
| mean anomaly at epoch: | 85.8332° |
| orbit number at epoch: | 24690 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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