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 52574U 26145.26981058 +.00000000 +00000-0 +14186-3 0 00006
2 52574 53.2133 135.3382 0001195 100.9098 259.2029 15.08829387 00
| Epoch (UTC): | 25 May 2026 06:28:31 |
| Eccentricity: | 0.0001195 |
| inclination: | 53.2133° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 135.3382° |
| argument of perigee: | 100.9098° |
| revolutions per day: | 15.08829387 |
| mean anomaly at epoch: | 259.2029° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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