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 55304U 26145.52859161 +.00000000 +00000-0 +57846-4 0 00009
2 55304 69.9989 190.5233 0003775 267.3228 92.7499 14.98330464 06
| Epoch (UTC): | 25 May 2026 12:41:10 |
| Eccentricity: | 0.0003775 |
| inclination: | 69.9989° |
| perigee height: | 569 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 190.5233° |
| argument of perigee: | 267.3228° |
| revolutions per day: | 14.98330464 |
| mean anomaly at epoch: | 92.7499° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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