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 64835U 26145.39694220 +.00000000 +00000-0 +12578-3 0 00008
2 64835 51.8991 298.9096 0000742 132.0507 228.0519 14.79936034 08
| Epoch (UTC): | 25 May 2026 09:31:35 |
| Eccentricity: | 0.0000742 |
| inclination: | 51.8991° |
| perigee height: | 629 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 298.9096° |
| argument of perigee: | 132.0507° |
| revolutions per day: | 14.79936034 |
| mean anomaly at epoch: | 228.0519° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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