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 64523U 26145.27123470 +.00000000 +00000-0 +60378-3 0 00004
2 64523 51.9035 259.4745 0001317 105.3764 254.7344 14.79960644 08
| Epoch (UTC): | 25 May 2026 06:30:34 |
| Eccentricity: | 0.0001317 |
| inclination: | 51.9035° |
| perigee height: | 629 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 259.4745° |
| argument of perigee: | 105.3764° |
| revolutions per day: | 14.79960644 |
| mean anomaly at epoch: | 254.7344° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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