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 64321U 26144.87320160 +.00000000 +00000-0 +14010-2 0 00001
2 64321 42.9984 290.2235 0001379 271.3044 88.7666 15.70956062 00
| Epoch (UTC): | 24 May 2026 20:57:24 |
| Eccentricity: | 0.0001379 |
| inclination: | 42.9984° |
| perigee height: | 355 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 290.2235° |
| argument of perigee: | 271.3044° |
| revolutions per day: | 15.70956062 |
| mean anomaly at epoch: | 88.7666° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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