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 65744U 26145.54798274 +.00000000 +00000-0 +65256-3 0 00000
2 65744 53.1576 335.7003 0001209 92.9120 267.2019 15.30207665 03
| Epoch (UTC): | 25 May 2026 13:09:05 |
| Eccentricity: | 0.0001209 |
| inclination: | 53.1576° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 335.7003° |
| argument of perigee: | 92.9120° |
| revolutions per day: | 15.30207665 |
| mean anomaly at epoch: | 267.2019° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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