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 52737U 26145.54165580 +.00000000 +00000-0 +18989-3 0 00007
2 52737 97.6566 290.3589 0006052 188.3886 171.7256 15.34019782 05
| Epoch (UTC): | 25 May 2026 12:59:59 |
| Eccentricity: | 0.0006052 |
| inclination: | 97.6566° |
| perigee height: | 460 km |
| apogee height: | 468 km |
| right ascension of ascending node: | 290.3589° |
| argument of perigee: | 188.3886° |
| revolutions per day: | 15.34019782 |
| mean anomaly at epoch: | 171.7256° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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