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 53128U 26145.58939263 +.00000000 +00000-0 +70625-5 0 00000
2 53128 97.3930 155.8402 0001660 91.1510 268.9918 15.24497704 03
| Epoch (UTC): | 25 May 2026 14:08:43 |
| Eccentricity: | 0.0001660 |
| inclination: | 97.3930° |
| perigee height: | 491 km |
| apogee height: | 493 km |
| right ascension of ascending node: | 155.8402° |
| argument of perigee: | 91.1510° |
| revolutions per day: | 15.24497704 |
| mean anomaly at epoch: | 268.9918° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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