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 64193U 26145.27253101 +.00000000 +00000-0 +96711-3 0 00002
2 64193 53.1599 94.4659 0001291 103.8730 256.2416 15.34387322 03
| Epoch (UTC): | 25 May 2026 06:32:26 |
| Eccentricity: | 0.0001291 |
| inclination: | 53.1599° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 94.4659° |
| argument of perigee: | 103.8730° |
| revolutions per day: | 15.34387322 |
| mean anomaly at epoch: | 256.2416° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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