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 67722U 26145.56711340 +.00000000 +00000-0 +60069-3 0 00006
2 67722 97.2851 199.0218 0000780 235.5918 124.5251 15.33462168 05
| Epoch (UTC): | 25 May 2026 13:36:38 |
| Eccentricity: | 0.0000780 |
| inclination: | 97.2851° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 199.0218° |
| argument of perigee: | 235.5918° |
| revolutions per day: | 15.33462168 |
| mean anomaly at epoch: | 124.5251° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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