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 64685U 26145.24601758 +.00000000 +00000-0 +74021-3 0 00000
2 64685 53.1562 130.8425 0001098 81.8118 278.3009 15.34399108 03
| Epoch (UTC): | 25 May 2026 05:54:15 |
| Eccentricity: | 0.0001098 |
| inclination: | 53.1562° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 130.8425° |
| argument of perigee: | 81.8118° |
| revolutions per day: | 15.34399108 |
| mean anomaly at epoch: | 278.3009° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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