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 66606U 26145.55599221 +.00000000 +00000-0 +77439-3 0 00006
2 66606 42.9993 341.8954 0001895 271.6983 88.3651 15.27596503 09
| Epoch (UTC): | 25 May 2026 13:20:37 |
| Eccentricity: | 0.0001895 |
| inclination: | 42.9993° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 341.8954° |
| argument of perigee: | 271.6983° |
| revolutions per day: | 15.27596503 |
| mean anomaly at epoch: | 88.3651° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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