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 67560U 26145.64693455 +.00000000 +00000-0 +45721-3 0 00009
2 67560 97.2873 32.7826 0002187 97.4108 262.7383 15.33455998 00
| Epoch (UTC): | 25 May 2026 15:31:35 |
| Eccentricity: | 0.0002187 |
| inclination: | 97.2873° |
| perigee height: | 464 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 32.7826° |
| argument of perigee: | 97.4108° |
| revolutions per day: | 15.33455998 |
| mean anomaly at epoch: | 262.7383° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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