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 66078U 26145.56989612 +.00000000 +00000-0 +26628-3 0 00001
2 66078 53.1585 248.0620 0000817 68.2316 291.8772 15.30196469 00
| Epoch (UTC): | 25 May 2026 13:40:39 |
| Eccentricity: | 0.0000817 |
| inclination: | 53.1585° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 248.0620° |
| argument of perigee: | 68.2316° |
| revolutions per day: | 15.30196469 |
| mean anomaly at epoch: | 291.8772° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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