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 45747U 26145.55370816 +.00000000 +00000-0 +20771-3 0 00003
2 45747 53.0764 206.2581 0003182 120.6622 239.4691 15.28029620 00
| Epoch (UTC): | 25 May 2026 13:17:20 |
| Eccentricity: | 0.0003182 |
| inclination: | 53.0764° |
| perigee height: | 480 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 206.2581° |
| argument of perigee: | 120.6622° |
| revolutions per day: | 15.28029620 |
| mean anomaly at epoch: | 239.4691° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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