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 66007U 26145.27609484 +.00000000 +00000-0 +43754-3 0 00006
2 66007 53.1599 108.0015 0001221 89.5515 270.5626 15.30204563 04
| Epoch (UTC): | 25 May 2026 06:37:34 |
| Eccentricity: | 0.0001221 |
| inclination: | 53.1599° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 108.0015° |
| argument of perigee: | 89.5515° |
| revolutions per day: | 15.30204563 |
| mean anomaly at epoch: | 270.5626° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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