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 66067U 26144.99895170 +.00000000 +00000-0 +42572-3 0 00006
2 66067 53.1593 250.8980 0001387 73.3166 286.7987 15.30197555 08
| Epoch (UTC): | 24 May 2026 23:58:29 |
| Eccentricity: | 0.0001387 |
| inclination: | 53.1593° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 250.8980° |
| argument of perigee: | 73.3166° |
| revolutions per day: | 15.30197555 |
| mean anomaly at epoch: | 286.7987° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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