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 55307U 26145.36567272 +.00000000 +00000-0 +54286-4 0 00008
2 55307 69.9983 171.2875 0003880 265.1615 94.9101 14.98333213 03
| Epoch (UTC): | 25 May 2026 08:46:34 |
| Eccentricity: | 0.0003880 |
| inclination: | 69.9983° |
| perigee height: | 569 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 171.2875° |
| argument of perigee: | 265.1615° |
| revolutions per day: | 14.98333213 |
| mean anomaly at epoch: | 94.9101° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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