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 64904U 26145.26144086 +.00000000 +00000-0 +12382-1 0 00002
2 64904 53.1599 350.2642 0002842 172.9125 187.1917 15.31841428 03
| Epoch (UTC): | 25 May 2026 06:16:28 |
| Eccentricity: | 0.0002842 |
| inclination: | 53.1599° |
| perigee height: | 468 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 350.2642° |
| argument of perigee: | 172.9125° |
| revolutions per day: | 15.31841428 |
| mean anomaly at epoch: | 187.1917° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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