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 65929U 26145.46902713 +.00000000 +00000-0 +37428-3 0 00001
2 65929 53.1589 169.0249 0001204 87.1604 272.9534 15.30194654 08
| Epoch (UTC): | 25 May 2026 11:15:23 |
| Eccentricity: | 0.0001204 |
| inclination: | 53.1589° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 169.0249° |
| argument of perigee: | 87.1604° |
| revolutions per day: | 15.30194654 |
| mean anomaly at epoch: | 272.9534° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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