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 65923U 26145.45319934 +.00000000 +00000-0 +48026-3 0 00007
2 65923 53.1595 168.9264 0001224 72.3302 287.7833 15.30207005 08
| Epoch (UTC): | 25 May 2026 10:52:36 |
| Eccentricity: | 0.0001224 |
| inclination: | 53.1595° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 168.9264° |
| argument of perigee: | 72.3302° |
| revolutions per day: | 15.30207005 |
| mean anomaly at epoch: | 287.7833° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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