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 66073U 26145.54363135 +.00000000 +00000-0 +80150-3 0 00000
2 66073 53.1603 248.6101 0001884 88.9642 271.1575 15.30206500 02
| Epoch (UTC): | 25 May 2026 13:02:49 |
| Eccentricity: | 0.0001884 |
| inclination: | 53.1603° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 248.6101° |
| argument of perigee: | 88.9642° |
| revolutions per day: | 15.30206500 |
| mean anomaly at epoch: | 271.1575° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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