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 64665U 26145.36157208 +.00000000 +00000-0 +11028-2 0 00004
2 64665 53.1591 130.1521 0001352 96.7639 263.3517 15.34385200 05
| Epoch (UTC): | 25 May 2026 08:40:39 |
| Eccentricity: | 0.0001352 |
| inclination: | 53.1591° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 130.1521° |
| argument of perigee: | 96.7639° |
| revolutions per day: | 15.34385200 |
| mean anomaly at epoch: | 263.3517° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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