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 63666U 26145.45344902 +.00000000 +00000-0 +16973-2 0 00007
2 63666 42.9871 166.7622 0009664 103.2970 256.8990 16.10337525 09
| Epoch (UTC): | 25 May 2026 10:52:57 |
| Eccentricity: | 0.0009664 |
| inclination: | 42.9871° |
| perigee height: | 240 km |
| apogee height: | 252 km |
| right ascension of ascending node: | 166.7622° |
| argument of perigee: | 103.2970° |
| revolutions per day: | 16.10337525 |
| mean anomaly at epoch: | 256.8990° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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