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 64820U 26145.20115222 +.00000000 +00000-0 +17355-3 0 00000
2 64820 51.9000 324.7429 0000734 120.8221 239.2813 14.79935953 01
| Epoch (UTC): | 25 May 2026 04:49:39 |
| Eccentricity: | 0.0000734 |
| inclination: | 51.9000° |
| perigee height: | 629 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 324.7429° |
| argument of perigee: | 120.8221° |
| revolutions per day: | 14.79935953 |
| mean anomaly at epoch: | 239.2813° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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