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 66673U 26144.64037904 +.00000000 +00000-0 +63674-3 0 00000
2 66673 97.4164 218.7610 0007751 100.5124 259.6986 15.22236975 06
| Epoch (UTC): | 24 May 2026 15:22:08 |
| Eccentricity: | 0.0007751 |
| inclination: | 97.4164° |
| perigee height: | 494 km |
| apogee height: | 504 km |
| right ascension of ascending node: | 218.7610° |
| argument of perigee: | 100.5124° |
| revolutions per day: | 15.22236975 |
| mean anomaly at epoch: | 259.6986° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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