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 55015U 26145.59729080 +.00000000 +00000-0 +22322-3 0 00001
2 55015 97.3355 213.5155 0007133 172.1071 188.0288 15.39616528 06
| Epoch (UTC): | 25 May 2026 14:20:05 |
| Eccentricity: | 0.0007133 |
| inclination: | 97.3355° |
| perigee height: | 442 km |
| apogee height: | 452 km |
| right ascension of ascending node: | 213.5155° |
| argument of perigee: | 172.1071° |
| revolutions per day: | 15.39616528 |
| mean anomaly at epoch: | 188.0288° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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