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 64493U 26145.24977272 +.00000000 +00000-0 +73116-3 0 00008
2 64493 53.1603 118.7988 0001392 75.1338 284.9819 15.35398063 04
| Epoch (UTC): | 25 May 2026 05:59:40 |
| Eccentricity: | 0.0001392 |
| inclination: | 53.1603° |
| perigee height: | 459 km |
| apogee height: | 461 km |
| right ascension of ascending node: | 118.7988° |
| argument of perigee: | 75.1338° |
| revolutions per day: | 15.35398063 |
| mean anomaly at epoch: | 284.9819° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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