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 64096U 26145.65833674 +.00000000 +00000-0 +44396-3 0 00007
2 64096 53.1608 29.4702 0001409 87.9838 272.1324 15.30213299 07
| Epoch (UTC): | 25 May 2026 15:48:00 |
| Eccentricity: | 0.0001409 |
| inclination: | 53.1608° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 29.4702° |
| argument of perigee: | 87.9838° |
| revolutions per day: | 15.30213299 |
| mean anomaly at epoch: | 272.1324° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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