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 57378U 26145.36600214 +.00000000 +00000-0 +15725-4 0 00007
2 57378 43.0025 139.4340 0000752 265.4725 94.6041 15.27577110 05
| Epoch (UTC): | 25 May 2026 08:47:02 |
| Eccentricity: | 0.0000752 |
| inclination: | 43.0025° |
| perigee height: | 483 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 139.4340° |
| argument of perigee: | 265.4725° |
| revolutions per day: | 15.27577110 |
| mean anomaly at epoch: | 94.6041° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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