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 67596U 26145.42888839 +.00000000 +00000-0 +62814-3 0 00008
2 67596 97.2855 210.5367 0000043 111.3389 248.7858 15.33449449 06
| Epoch (UTC): | 25 May 2026 10:17:35 |
| Eccentricity: | 0.0000043 |
| inclination: | 97.2855° |
| perigee height: | 466 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 210.5367° |
| argument of perigee: | 111.3389° |
| revolutions per day: | 15.33449449 |
| mean anomaly at epoch: | 248.7858° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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