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 66159U 26145.50189720 +.00000000 +00000-0 +63582-3 0 00007
2 66159 53.1604 65.6830 0001112 85.1832 274.9298 15.34400077 00
| Epoch (UTC): | 25 May 2026 12:02:43 |
| Eccentricity: | 0.0001112 |
| inclination: | 53.1604° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 65.6830° |
| argument of perigee: | 85.1832° |
| revolutions per day: | 15.34400077 |
| mean anomaly at epoch: | 274.9298° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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