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 52543U 26145.26520543 +.00000000 +00000-0 -26988-4 0 00005
2 52543 53.2136 145.3577 0000950 85.6790 274.4311 15.08845546 00
| Epoch (UTC): | 25 May 2026 06:21:53 |
| Eccentricity: | 0.0000950 |
| inclination: | 53.2136° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 145.3577° |
| argument of perigee: | 85.6790° |
| revolutions per day: | 15.08845546 |
| mean anomaly at epoch: | 274.4311° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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