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 52292U 26145.19068286 +.00000000 +00000-0 +18498-4 0 00005
2 52292 53.2125 115.6934 0001307 75.6702 284.4435 15.08842636 00
| Epoch (UTC): | 25 May 2026 04:34:34 |
| Eccentricity: | 0.0001307 |
| inclination: | 53.2125° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 115.6934° |
| argument of perigee: | 75.6702° |
| revolutions per day: | 15.08842636 |
| mean anomaly at epoch: | 284.4435° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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