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 65747U 26145.50060885 +.00000000 +00000-0 +59670-3 0 00002
2 65747 53.1595 336.1132 0001548 91.2567 268.8611 15.30205604 04
| Epoch (UTC): | 25 May 2026 12:00:52 |
| Eccentricity: | 0.0001548 |
| inclination: | 53.1595° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 336.1132° |
| argument of perigee: | 91.2567° |
| revolutions per day: | 15.30205604 |
| mean anomaly at epoch: | 268.8611° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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