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 53323U 26145.56051053 +.00000000 +00000-0 +71549-3 0 00001
2 53323 97.2250 248.7835 0002165 153.3930 206.7444 15.70427358 07
| Epoch (UTC): | 25 May 2026 13:27:08 |
| Eccentricity: | 0.0002165 |
| inclination: | 97.2250° |
| perigee height: | 356 km |
| apogee height: | 359 km |
| right ascension of ascending node: | 248.7835° |
| argument of perigee: | 153.3930° |
| revolutions per day: | 15.70427358 |
| mean anomaly at epoch: | 206.7444° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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