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 66123U 26145.43760961 +.00000000 +00000-0 +40435-3 0 00004
2 66123 53.1592 42.9458 0001086 82.1889 277.9235 15.30211841 09
| Epoch (UTC): | 25 May 2026 10:30:09 |
| Eccentricity: | 0.0001086 |
| inclination: | 53.1592° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 42.9458° |
| argument of perigee: | 82.1889° |
| revolutions per day: | 15.30211841 |
| mean anomaly at epoch: | 277.9235° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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