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 66514U 26145.36573020 +.00000000 +00000-0 +66272-4 0 00006
2 66514 66.0392 182.5796 0008056 269.3823 90.6269 12.80929091 03
| Epoch (UTC): | 25 May 2026 08:46:39 |
| Eccentricity: | 0.0008056 |
| inclination: | 66.0392° |
| perigee height: | 1332 km |
| apogee height: | 1344 km |
| right ascension of ascending node: | 182.5796° |
| argument of perigee: | 269.3823° |
| revolutions per day: | 12.80929091 |
| mean anomaly at epoch: | 90.6269° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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