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 26099.84309367 +.00000000 +00000-0 +13979-3 0 00007
2 14966 82.9724 240.1945 0017459 85.1355 70.9072 13.74887346 04
| Epoch (UTC): | 09 April 2026 20:14:03 |
| Eccentricity: | 0.0017459 |
| inclination: | 82.9724° |
| perigee height: | 969 km |
| apogee height: | 995 km |
| right ascension of ascending node: | 240.1945° |
| argument of perigee: | 85.1355° |
| revolutions per day: | 13.74887346 |
| mean anomaly at epoch: | 70.9072° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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