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 56520U 26145.35190995 +.00000000 +00000-0 -58766-6 0 00009
2 56520 43.0007 139.5757 0000990 277.8091 82.2648 15.27571930 03
| Epoch (UTC): | 25 May 2026 08:26:45 |
| Eccentricity: | 0.0000990 |
| inclination: | 43.0007° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 139.5757° |
| argument of perigee: | 277.8091° |
| revolutions per day: | 15.27571930 |
| mean anomaly at epoch: | 82.2648° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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