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 27665U 26020.93709659 +.00000000 +00000-0 +15926-3 0 00003
2 27665 39.5768 315.9578 0008862 172.7489 263.9188 14.29503231 03
| Epoch (UTC): | 20 January 2026 22:29:25 |
| Eccentricity: | 0.0008862 |
| inclination: | 39.5768° |
| perigee height: | 787 km |
| apogee height: | 800 km |
| right ascension of ascending node: | 315.9578° |
| argument of perigee: | 172.7489° |
| revolutions per day: | 14.29503231 |
| mean anomaly at epoch: | 263.9188° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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