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 14966U 26088.20242670 +.00000000 +00000-0 +19573-3 0 00004
2 14966 82.9704 248.7808 0017381 115.0586 56.9597 13.74884228 09
| Epoch (UTC): | 29 March 2026 04:51:29 |
| Eccentricity: | 0.0017381 |
| inclination: | 82.9704° |
| perigee height: | 969 km |
| apogee height: | 995 km |
| right ascension of ascending node: | 248.7808° |
| argument of perigee: | 115.0586° |
| revolutions per day: | 13.74884228 |
| mean anomaly at epoch: | 56.9597° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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