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 26106.74496479 +.00000000 +00000-0 +19179-4 0 00005
2 27665 39.5751 238.2700 0008961 356.0157 151.4735 14.29540282 04
| Epoch (UTC): | 16 April 2026 17:52:44 |
| Eccentricity: | 0.0008961 |
| inclination: | 39.5751° |
| perigee height: | 787 km |
| apogee height: | 800 km |
| right ascension of ascending node: | 238.2700° |
| argument of perigee: | 356.0157° |
| revolutions per day: | 14.29540282 |
| mean anomaly at epoch: | 151.4735° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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