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 66801U 26145.12061447 +.00000000 +00000-0 +86115-3 0 00001
2 66801 43.0016 43.1215 0001344 258.6713 101.3988 15.27606174 06
| Epoch (UTC): | 25 May 2026 02:53:41 |
| Eccentricity: | 0.0001344 |
| inclination: | 43.0016° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 43.1215° |
| argument of perigee: | 258.6713° |
| revolutions per day: | 15.27606174 |
| mean anomaly at epoch: | 101.3988° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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