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 66288U 26145.40617014 +.00000000 +00000-0 +51732-3 0 00005
2 66288 53.1590 194.0829 0001215 78.9399 281.1741 15.34405559 07
| Epoch (UTC): | 25 May 2026 09:44:53 |
| Eccentricity: | 0.0001215 |
| inclination: | 53.1590° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 194.0829° |
| argument of perigee: | 78.9399° |
| revolutions per day: | 15.34405559 |
| mean anomaly at epoch: | 281.1741° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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