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 64267U 26145.58335647 +.00000000 +00000-0 -62372-3 0 00001
2 64267 53.1599 117.1180 0000740 102.8204 229.2575 15.34401228 08
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0000740 |
| inclination: | 53.1599° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 117.1180° |
| argument of perigee: | 102.8204° |
| revolutions per day: | 15.34401228 |
| mean anomaly at epoch: | 229.2575° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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