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 64081U 26145.41608932 +.00000000 +00000-0 +84074-3 0 00009
2 64081 43.0001 128.3343 0001985 253.1965 106.8669 15.27600083 05
| Epoch (UTC): | 25 May 2026 09:59:10 |
| Eccentricity: | 0.0001985 |
| inclination: | 43.0001° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 128.3343° |
| argument of perigee: | 253.1965° |
| revolutions per day: | 15.27600083 |
| mean anomaly at epoch: | 106.8669° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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