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 64892U 26145.60864588 +.00000000 +00000-0 +45103-3 0 00001
2 64892 97.4534 114.8713 0003761 257.9401 102.1419 15.32698724 08
| Epoch (UTC): | 25 May 2026 14:36:27 |
| Eccentricity: | 0.0003761 |
| inclination: | 97.4534° |
| perigee height: | 465 km |
| apogee height: | 470 km |
| right ascension of ascending node: | 114.8713° |
| argument of perigee: | 257.9401° |
| revolutions per day: | 15.32698724 |
| mean anomaly at epoch: | 102.1419° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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