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 66571U 26145.37750959 +.00000000 +00000-0 +82847-3 0 00003
2 66571 42.9968 274.3659 0000200 257.1141 102.9689 15.27602228 04
| Epoch (UTC): | 25 May 2026 09:03:36 |
| Eccentricity: | 0.0000200 |
| inclination: | 42.9968° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 274.3659° |
| argument of perigee: | 257.1141° |
| revolutions per day: | 15.27602228 |
| mean anomaly at epoch: | 102.9689° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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