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 66858U 26145.64459704 +.00000000 +00000-0 +55984-3 0 00007
2 66858 42.9999 268.9715 0000494 338.3213 21.7618 15.27586283 07
| Epoch (UTC): | 25 May 2026 15:28:13 |
| Eccentricity: | 0.0000494 |
| inclination: | 42.9999° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 268.9715° |
| argument of perigee: | 338.3213° |
| revolutions per day: | 15.27586283 |
| mean anomaly at epoch: | 21.7618° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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