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 64003U 26145.08756022 +.00000000 +00000-0 +54055-3 0 00006
2 64003 42.9956 286.1345 0001824 55.8954 304.2070 15.27585823 02
| Epoch (UTC): | 25 May 2026 02:06:05 |
| Eccentricity: | 0.0001824 |
| inclination: | 42.9956° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 286.1345° |
| argument of perigee: | 55.8954° |
| revolutions per day: | 15.27585823 |
| mean anomaly at epoch: | 304.2070° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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