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 64133U 26145.60808252 +.00000000 +00000-0 +21437-2 0 00008
2 64133 42.9997 230.4500 0001317 303.2153 56.8589 15.70874705 07
| Epoch (UTC): | 25 May 2026 14:35:38 |
| Eccentricity: | 0.0001317 |
| inclination: | 42.9997° |
| perigee height: | 356 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 230.4500° |
| argument of perigee: | 303.2153° |
| revolutions per day: | 15.70874705 |
| mean anomaly at epoch: | 56.8589° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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