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 64676U 26145.39093036 +.00000000 +00000-0 +51961-3 0 00008
2 64676 53.1575 129.6192 0001583 81.7137 278.4045 15.34390599 09
| Epoch (UTC): | 25 May 2026 09:22:56 |
| Eccentricity: | 0.0001583 |
| inclination: | 53.1575° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 129.6192° |
| argument of perigee: | 81.7137° |
| revolutions per day: | 15.34390599 |
| mean anomaly at epoch: | 278.4045° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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