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 64328U 26145.10630870 +.00000000 +00000-0 +13484-2 0 00001
2 64328 42.9989 288.5167 0000470 353.2204 6.8658 15.70894121 04
| Epoch (UTC): | 25 May 2026 02:33:05 |
| Eccentricity: | 0.0000470 |
| inclination: | 42.9989° |
| perigee height: | 356 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 288.5167° |
| argument of perigee: | 353.2204° |
| revolutions per day: | 15.70894121 |
| mean anomaly at epoch: | 6.8658° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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