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 25346.90696968 .00000248 00000-0 94177-4 0 9996
2 27386 98.3600 297.6432 0001131 83.1345 345.5905 14.38999439246694
| Epoch (UTC): | 12 December 2025 21:46:02 |
| Eccentricity: | 0.0001131 |
| inclination: | 98.3600° |
| perigee height: | 761 km |
| apogee height: | 762 km |
| right ascension of ascending node: | 297.6432° |
| argument of perigee: | 83.1345° |
| revolutions per day: | 14.38999439 |
| mean anomaly at epoch: | 345.5905° |
| orbit number at epoch: | 24669 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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