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 67651U 26145.05465014 +.00000000 +00000-0 +51859-3 0 00002
2 67651 97.2847 178.2791 0001184 94.6994 265.4384 15.33457359 01
| Epoch (UTC): | 25 May 2026 01:18:41 |
| Eccentricity: | 0.0001184 |
| inclination: | 97.2847° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 178.2791° |
| argument of perigee: | 94.6994° |
| revolutions per day: | 15.33457359 |
| mean anomaly at epoch: | 265.4384° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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