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 64143U 26145.30322348 +.00000000 +00000-0 +74719-3 0 00005
2 64143 43.0008 4.9192 0001456 269.5565 90.5120 15.27596715 09
| Epoch (UTC): | 25 May 2026 07:16:38 |
| Eccentricity: | 0.0001456 |
| inclination: | 43.0008° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 4.9192° |
| argument of perigee: | 269.5565° |
| revolutions per day: | 15.27596715 |
| mean anomaly at epoch: | 90.5120° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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