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 64176U 26145.54570469 +.00000000 +00000-0 +85288-3 0 00009
2 64176 53.1584 93.3233 0001239 85.9191 274.1953 15.34408569 09
| Epoch (UTC): | 25 May 2026 13:05:48 |
| Eccentricity: | 0.0001239 |
| inclination: | 53.1584° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 93.3233° |
| argument of perigee: | 85.9191° |
| revolutions per day: | 15.34408569 |
| mean anomaly at epoch: | 274.1953° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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