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 66716U 26145.13134017 +.00000000 +00000-0 +25556-3 0 00003
2 66716 97.4226 219.3242 0002252 68.4909 291.6567 15.20389760 05
| Epoch (UTC): | 25 May 2026 03:09:07 |
| Eccentricity: | 0.0002252 |
| inclination: | 97.4226° |
| perigee height: | 503 km |
| apogee height: | 506 km |
| right ascension of ascending node: | 219.3242° |
| argument of perigee: | 68.4909° |
| revolutions per day: | 15.20389760 |
| mean anomaly at epoch: | 291.6567° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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