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 66612U 26144.86372850 +.00000000 +00000-0 +46250-3 0 00000
2 66612 43.0023 346.1677 0001378 267.0996 92.9698 15.27607972 06
| Epoch (UTC): | 24 May 2026 20:43:46 |
| Eccentricity: | 0.0001378 |
| inclination: | 43.0023° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 346.1677° |
| argument of perigee: | 267.0996° |
| revolutions per day: | 15.27607972 |
| mean anomaly at epoch: | 92.9698° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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