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 26039.51245237 +.00000000 +00000-0 +64337-4 0 00005
2 27665 39.5737 221.2105 0010012 284.8380 105.9763 14.29513588 09
| Epoch (UTC): | 08 February 2026 12:17:55 |
| Eccentricity: | 0.0010012 |
| inclination: | 39.5737° |
| perigee height: | 786 km |
| apogee height: | 801 km |
| right ascension of ascending node: | 221.2105° |
| argument of perigee: | 284.8380° |
| revolutions per day: | 14.29513588 |
| mean anomaly at epoch: | 105.9763° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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