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 61531U 26145.28206500 +.00000000 +00000-0 +33203-4 0 00005
2 61531 53.1593 144.2334 0000866 78.4868 281.6235 15.42165753 02
| Epoch (UTC): | 25 May 2026 06:46:10 |
| Eccentricity: | 0.0000866 |
| inclination: | 53.1593° |
| perigee height: | 439 km |
| apogee height: | 440 km |
| right ascension of ascending node: | 144.2334° |
| argument of perigee: | 78.4868° |
| revolutions per day: | 15.42165753 |
| mean anomaly at epoch: | 281.6235° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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