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 66662U 26145.52884100 +.00000000 +00000-0 +15415-3 0 00004
2 66662 97.7487 75.3437 0016545 93.8839 266.4273 14.94080069 01
| Epoch (UTC): | 25 May 2026 12:41:31 |
| Eccentricity: | 0.0016545 |
| inclination: | 97.7487° |
| perigee height: | 574 km |
| apogee height: | 597 km |
| right ascension of ascending node: | 75.3437° |
| argument of perigee: | 93.8839° |
| revolutions per day: | 14.94080069 |
| mean anomaly at epoch: | 266.4273° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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