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 40063U 26145.61277426 +.00000000 +00000-0 -48844-4 0 00002
2 40063 82.5104 321.7000 0021698 188.9761 171.0934 12.42944750 07
| Epoch (UTC): | 25 May 2026 14:42:23 |
| Eccentricity: | 0.0021698 |
| inclination: | 82.5104° |
| perigee height: | 1477 km |
| apogee height: | 1511 km |
| right ascension of ascending node: | 321.7000° |
| argument of perigee: | 188.9761° |
| revolutions per day: | 12.42944750 |
| mean anomaly at epoch: | 171.0934° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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