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 64604U 26144.95545329 +.00000000 +00000-0 +99390-3 0 00005
2 64604 53.1596 340.8394 0000992 84.1912 275.9202 15.30203330 04
| Epoch (UTC): | 24 May 2026 22:55:51 |
| Eccentricity: | 0.0000992 |
| inclination: | 53.1596° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 340.8394° |
| argument of perigee: | 84.1912° |
| revolutions per day: | 15.30203330 |
| mean anomaly at epoch: | 275.9202° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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