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 26039.56271427 +.00000000 +00000-0 +47021-4 0 00002
2 27387 98.8167 54.6783 0032708 144.2892 216.0490 14.36762730 02
| Epoch (UTC): | 08 February 2026 13:30:18 |
| Eccentricity: | 0.0032708 |
| inclination: | 98.8167° |
| perigee height: | 746 km |
| apogee height: | 793 km |
| right ascension of ascending node: | 54.6783° |
| argument of perigee: | 144.2892° |
| revolutions per day: | 14.36762730 |
| mean anomaly at epoch: | 216.0490° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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