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 65748U 26145.24462756 +.00000000 +00000-0 +81993-3 0 00000
2 65748 53.1598 337.3641 0001183 92.2762 267.8374 15.30196746 00
| Epoch (UTC): | 25 May 2026 05:52:15 |
| Eccentricity: | 0.0001183 |
| inclination: | 53.1598° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 337.3641° |
| argument of perigee: | 92.2762° |
| revolutions per day: | 15.30196746 |
| mean anomaly at epoch: | 267.8374° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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