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 is defined by the following mean orbital elements,
1 27387U 26039.63235513 +.00000000 +00000-0 +47044-4 0 00001
2 27387 98.8167 54.7496 0032709 144.0861 216.2531 14.36762741 09
| Epoch (UTC): | 08 February 2026 15:10:35 |
| Eccentricity: | 0.0032709 |
| inclination: | 98.8167° |
| perigee height: | 746 km |
| apogee height: | 793 km |
| right ascension of ascending node: | 54.7496° |
| argument of perigee: | 144.0861° |
| revolutions per day: | 14.36762741 |
| mean anomaly at epoch: | 216.2531° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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