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 65729U 26031.05194253 +.00000000 +00000-0 +96629-3 0 00008
2 65729 51.6000 237.6139 0006569 265.0285 94.9990 16.36242872 09
| Epoch (UTC): | 31 January 2026 01:14:47 |
| Eccentricity: | 0.0006569 |
| inclination: | 51.6000° |
| perigee height: | 172 km |
| apogee height: | 180 km |
| right ascension of ascending node: | 237.6139° |
| argument of perigee: | 265.0285° |
| revolutions per day: | 16.36242872 |
| mean anomaly at epoch: | 94.9990° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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