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 64317U 26144.87849713 +.00000000 +00000-0 +13328-2 0 00007
2 64317 42.9994 290.2677 0004122 239.5103 120.5358 15.70885053 01
| Epoch (UTC): | 24 May 2026 21:05:02 |
| Eccentricity: | 0.0004122 |
| inclination: | 42.9994° |
| perigee height: | 354 km |
| apogee height: | 359 km |
| right ascension of ascending node: | 290.2677° |
| argument of perigee: | 239.5103° |
| revolutions per day: | 15.70885053 |
| mean anomaly at epoch: | 120.5358° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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