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 64015U 26145.42861661 +.00000000 +00000-0 +63854-3 0 00000
2 64015 42.9996 284.3899 0001152 281.8743 78.1979 15.27592172 04
| Epoch (UTC): | 25 May 2026 10:17:12 |
| Eccentricity: | 0.0001152 |
| inclination: | 42.9996° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 284.3899° |
| argument of perigee: | 281.8743° |
| revolutions per day: | 15.27592172 |
| mean anomaly at epoch: | 78.1979° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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