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 52296U 26145.30846137 +.00000000 +00000-0 +14008-3 0 00003
2 52296 53.2127 115.1682 0001577 64.2991 295.8164 15.08846947 08
| Epoch (UTC): | 25 May 2026 07:24:11 |
| Eccentricity: | 0.0001577 |
| inclination: | 53.2127° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 115.1682° |
| argument of perigee: | 64.2991° |
| revolutions per day: | 15.08846947 |
| mean anomaly at epoch: | 295.8164° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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