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 64340U 26145.50797336 +.00000000 +00000-0 +35679-3 0 00001
2 64340 42.0088 316.8031 0010427 334.1529 25.8776 15.01378623 05
| Epoch (UTC): | 25 May 2026 12:11:28 |
| Eccentricity: | 0.0010427 |
| inclination: | 42.0088° |
| perigee height: | 555 km |
| apogee height: | 570 km |
| right ascension of ascending node: | 316.8031° |
| argument of perigee: | 334.1529° |
| revolutions per day: | 15.01378623 |
| mean anomaly at epoch: | 25.8776° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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