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 66812U 26145.41928117 +.00000000 +00000-0 +69808-3 0 00001
2 66812 43.0044 41.0552 0001120 281.5777 78.4949 15.27597419 09
| Epoch (UTC): | 25 May 2026 10:03:45 |
| Eccentricity: | 0.0001120 |
| inclination: | 43.0044° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 41.0552° |
| argument of perigee: | 281.5777° |
| revolutions per day: | 15.27597419 |
| mean anomaly at epoch: | 78.4949° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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