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 67543U 26145.61973242 +.00000000 +00000-0 -25544-4 0 00005
2 67543 97.2859 32.6690 0002210 89.5074 270.6422 15.33438219 03
| Epoch (UTC): | 25 May 2026 14:52:24 |
| Eccentricity: | 0.0002210 |
| inclination: | 97.2859° |
| perigee height: | 464 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 32.6690° |
| argument of perigee: | 89.5074° |
| revolutions per day: | 15.33438219 |
| mean anomaly at epoch: | 270.6422° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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