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 15378U 26137.75244060 +.00000000 +00000-0 +68896-5 0 00006
2 15378 64.9898 140.0850 0045881 340.4949 19.4353 13.83710092 06
| Epoch (UTC): | 17 May 2026 18:03:30 |
| Eccentricity: | 0.0045881 |
| inclination: | 64.9898° |
| perigee height: | 917 km |
| apogee height: | 984 km |
| right ascension of ascending node: | 140.0850° |
| argument of perigee: | 340.4949° |
| revolutions per day: | 13.83710092 |
| mean anomaly at epoch: | 19.4353° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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