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 45665U 26145.57885660 +.00000000 +00000-0 +50721-3 0 00000
2 45665 53.0452 38.0109 0006580 65.8079 294.3623 15.66484587 05
| Epoch (UTC): | 25 May 2026 13:53:33 |
| Eccentricity: | 0.0006580 |
| inclination: | 53.0452° |
| perigee height: | 365 km |
| apogee height: | 373 km |
| right ascension of ascending node: | 38.0109° |
| argument of perigee: | 65.8079° |
| revolutions per day: | 15.66484587 |
| mean anomaly at epoch: | 294.3623° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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