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 26017.27756958 +.00000000 +00000-0 +38642-4 0 00002
2 27387 98.8164 31.8637 0031559 209.9751 149.9628 14.36754041 03
| Epoch (UTC): | 17 January 2026 06:39:42 |
| Eccentricity: | 0.0031559 |
| inclination: | 98.8164° |
| perigee height: | 747 km |
| apogee height: | 792 km |
| right ascension of ascending node: | 31.8637° |
| argument of perigee: | 209.9751° |
| revolutions per day: | 14.36754041 |
| mean anomaly at epoch: | 149.9628° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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