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 64095U 26145.76166595 +.00000000 +00000-0 +33358-3 0 00005
2 64095 72.9716 259.4304 0010272 159.4117 200.7494 15.28616012 03
| Epoch (UTC): | 25 May 2026 18:16:47 |
| Eccentricity: | 0.0010272 |
| inclination: | 72.9716° |
| perigee height: | 473 km |
| apogee height: | 487 km |
| right ascension of ascending node: | 259.4304° |
| argument of perigee: | 159.4117° |
| revolutions per day: | 15.28616012 |
| mean anomaly at epoch: | 200.7494° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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