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 45535U 26145.38702488 +.00000000 +00000-0 +28573-3 0 00001
2 45535 53.0722 32.4202 0001666 76.1822 283.9366 15.37902009 04
| Epoch (UTC): | 25 May 2026 09:17:18 |
| Eccentricity: | 0.0001666 |
| inclination: | 53.0722° |
| perigee height: | 451 km |
| apogee height: | 453 km |
| right ascension of ascending node: | 32.4202° |
| argument of perigee: | 76.1822° |
| revolutions per day: | 15.37902009 |
| mean anomaly at epoch: | 283.9366° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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