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 64494U 26145.33251414 +.00000000 +00000-0 +42163-3 0 00000
2 64494 53.1592 120.7294 0001219 96.3397 263.7743 15.30216226 09
| Epoch (UTC): | 25 May 2026 07:58:49 |
| Eccentricity: | 0.0001219 |
| inclination: | 53.1592° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 120.7294° |
| argument of perigee: | 96.3397° |
| revolutions per day: | 15.30216226 |
| mean anomaly at epoch: | 263.7743° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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