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 64450U 26145.25936325 +.00000000 +00000-0 +87744-3 0 00008
2 64450 53.1615 92.3528 0001877 96.8440 263.2777 15.34406668 02
| Epoch (UTC): | 25 May 2026 06:13:28 |
| Eccentricity: | 0.0001877 |
| inclination: | 53.1615° |
| perigee height: | 461 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 92.3528° |
| argument of perigee: | 96.8440° |
| revolutions per day: | 15.34406668 |
| mean anomaly at epoch: | 263.2777° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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