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 66156U 26145.49089161 +.00000000 +00000-0 +50709-3 0 00007
2 66156 53.1599 66.3206 0001652 90.1557 269.9633 15.30205897 00
| Epoch (UTC): | 25 May 2026 11:46:53 |
| Eccentricity: | 0.0001652 |
| inclination: | 53.1599° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 66.3206° |
| argument of perigee: | 90.1557° |
| revolutions per day: | 15.30205897 |
| mean anomaly at epoch: | 269.9633° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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