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 65734U 26145.55959255 +.00000000 +00000-0 +99253-3 0 00002
2 65734 53.1592 335.7765 0002074 79.3445 280.7789 15.30223075 02
| Epoch (UTC): | 25 May 2026 13:25:48 |
| Eccentricity: | 0.0002074 |
| inclination: | 53.1592° |
| perigee height: | 474 km |
| apogee height: | 477 km |
| right ascension of ascending node: | 335.7765° |
| argument of perigee: | 79.3445° |
| revolutions per day: | 15.30223075 |
| mean anomaly at epoch: | 280.7789° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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