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 64831U 26145.18357784 +.00000000 +00000-0 +89039-4 0 00009
2 64831 51.9029 309.8947 0000736 121.9746 238.1288 14.79931142 09
| Epoch (UTC): | 25 May 2026 04:24:21 |
| Eccentricity: | 0.0000736 |
| inclination: | 51.9029° |
| perigee height: | 629 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 309.8947° |
| argument of perigee: | 121.9746° |
| revolutions per day: | 14.79931142 |
| mean anomaly at epoch: | 238.1288° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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