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 66686U 26145.14505490 +.00000000 +00000-0 +26071-3 0 00000
2 66686 97.4252 219.0641 0006922 82.7641 277.4380 15.19087663 00
| Epoch (UTC): | 25 May 2026 03:28:52 |
| Eccentricity: | 0.0006922 |
| inclination: | 97.4252° |
| perigee height: | 504 km |
| apogee height: | 513 km |
| right ascension of ascending node: | 219.0641° |
| argument of perigee: | 82.7641° |
| revolutions per day: | 15.19087663 |
| mean anomaly at epoch: | 277.4380° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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