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 45565U 26144.94294822 +.00000000 +00000-0 +47546-3 0 00004
2 45565 53.0464 24.9991 0007475 81.4298 278.7564 15.67614044 05
| Epoch (UTC): | 24 May 2026 22:37:50 |
| Eccentricity: | 0.0007475 |
| inclination: | 53.0464° |
| perigee height: | 361 km |
| apogee height: | 371 km |
| right ascension of ascending node: | 24.9991° |
| argument of perigee: | 81.4298° |
| revolutions per day: | 15.67614044 |
| mean anomaly at epoch: | 278.7564° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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