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 64384U 26145.38294507 +.00000000 +00000-0 +66781-3 0 00005
2 64384 42.9989 106.8875 0001174 263.6703 96.4015 15.27595910 02
| Epoch (UTC): | 25 May 2026 09:11:26 |
| Eccentricity: | 0.0001174 |
| inclination: | 42.9989° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 106.8875° |
| argument of perigee: | 263.6703° |
| revolutions per day: | 15.27595910 |
| mean anomaly at epoch: | 96.4015° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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