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 65736U 26145.49533174 +.00000000 +00000-0 +50286-3 0 00008
2 65736 53.1580 336.0858 0001217 99.7763 260.3375 15.30210522 03
| Epoch (UTC): | 25 May 2026 11:53:16 |
| Eccentricity: | 0.0001217 |
| inclination: | 53.1580° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 336.0858° |
| argument of perigee: | 99.7763° |
| revolutions per day: | 15.30210522 |
| mean anomaly at epoch: | 260.3375° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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