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 56288U 26145.34467110 +.00000000 +00000-0 -84186-4 0 00008
2 56288 43.0005 135.9972 0001607 287.3622 72.7054 15.27576841 04
| Epoch (UTC): | 25 May 2026 08:16:19 |
| Eccentricity: | 0.0001607 |
| inclination: | 43.0005° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 135.9972° |
| argument of perigee: | 287.3622° |
| revolutions per day: | 15.27576841 |
| mean anomaly at epoch: | 72.7054° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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