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 66688U 26145.46982860 +.00000000 +00000-0 +24142-3 0 00004
2 66688 97.4227 219.3377 0006547 82.9801 277.2178 15.19079077 09
| Epoch (UTC): | 25 May 2026 11:16:33 |
| Eccentricity: | 0.0006547 |
| inclination: | 97.4227° |
| perigee height: | 504 km |
| apogee height: | 513 km |
| right ascension of ascending node: | 219.3377° |
| argument of perigee: | 82.9801° |
| revolutions per day: | 15.19079077 |
| mean anomaly at epoch: | 277.2178° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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