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 57380U 26145.36985279 +.00000000 +00000-0 +11837-4 0 00007
2 57380 43.0030 139.4499 0001240 300.6540 59.4189 15.27575782 04
| Epoch (UTC): | 25 May 2026 08:52:35 |
| Eccentricity: | 0.0001240 |
| inclination: | 43.0030° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 139.4499° |
| argument of perigee: | 300.6540° |
| revolutions per day: | 15.27575782 |
| mean anomaly at epoch: | 59.4189° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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