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 66912U 26144.90752000 +.00000000 +00000-0 +90501-3 0 00005
2 66912 51.6220 36.5143 0004799 152.3505 207.7754 15.82853823 01
| Epoch (UTC): | 24 May 2026 21:46:49 |
| Eccentricity: | 0.0004799 |
| inclination: | 51.6220° |
| perigee height: | 319 km |
| apogee height: | 326 km |
| right ascension of ascending node: | 36.5143° |
| argument of perigee: | 152.3505° |
| revolutions per day: | 15.82853823 |
| mean anomaly at epoch: | 207.7754° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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