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 64545U 26145.57747169 +.00000000 +00000-0 +12856-3 0 00006
2 64545 97.4611 260.7877 0007539 227.2278 132.8323 15.19304633 02
| Epoch (UTC): | 25 May 2026 13:51:33 |
| Eccentricity: | 0.0007539 |
| inclination: | 97.4611° |
| perigee height: | 503 km |
| apogee height: | 513 km |
| right ascension of ascending node: | 260.7877° |
| argument of perigee: | 227.2278° |
| revolutions per day: | 15.19304633 |
| mean anomaly at epoch: | 132.8323° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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