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 64501U 26145.36717396 +.00000000 +00000-0 +12268-3 0 00001
2 64501 51.8975 264.1287 0000927 159.7457 200.3543 14.79947890 04
| Epoch (UTC): | 25 May 2026 08:48:43 |
| Eccentricity: | 0.0000927 |
| inclination: | 51.8975° |
| perigee height: | 629 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 264.1287° |
| argument of perigee: | 159.7457° |
| revolutions per day: | 14.79947890 |
| mean anomaly at epoch: | 200.3543° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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