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 64253U 26145.30040397 +.00000000 +00000-0 +73742-3 0 00003
2 64253 43.0025 234.5907 0001520 267.3760 92.6918 15.27592619 07
| Epoch (UTC): | 25 May 2026 07:12:34 |
| Eccentricity: | 0.0001520 |
| inclination: | 43.0025° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 234.5907° |
| argument of perigee: | 267.3760° |
| revolutions per day: | 15.27592619 |
| mean anomaly at epoch: | 92.6918° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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