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 57327U 23091BB 25215.94783005 .07226389 25611-5 16265-2 0 9999
2 57327 97.5142 290.0171 0015369 258.0341 101.9230 16.29874339114825
| Epoch (UTC): | 03 August 2025 22:44:52 |
| Eccentricity: | 0.0015369 |
| inclination: | 97.5142° |
| perigee height: | 183 km |
| apogee height: | 203 km |
| right ascension of ascending node: | 290.0171° |
| argument of perigee: | 258.0341° |
| revolutions per day: | 16.29874339 |
| mean anomaly at epoch: | 101.9230° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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