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 64757U 26145.26367567 +.00000000 +00000-0 +16313-2 0 00008
2 64757 53.1592 246.5052 0001099 101.0256 259.0870 15.34364230 06
| Epoch (UTC): | 25 May 2026 06:19:41 |
| Eccentricity: | 0.0001099 |
| inclination: | 53.1592° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 246.5052° |
| argument of perigee: | 101.0256° |
| revolutions per day: | 15.34364230 |
| mean anomaly at epoch: | 259.0870° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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