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 52549U 26145.38296826 +.00000000 +00000-0 -13525-4 0 00001
2 52549 53.2113 144.8303 0001034 63.6529 296.4569 15.08840822 03
| Epoch (UTC): | 25 May 2026 09:11:28 |
| Eccentricity: | 0.0001034 |
| inclination: | 53.2113° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 144.8303° |
| argument of perigee: | 63.6529° |
| revolutions per day: | 15.08840822 |
| mean anomaly at epoch: | 296.4569° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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