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 67797U 26145.08587459 +.00000000 +00000-0 +39521-3 0 00006
2 67797 97.2855 333.2559 0001601 88.3703 271.7724 15.33451934 09
| Epoch (UTC): | 25 May 2026 02:03:39 |
| Eccentricity: | 0.0001601 |
| inclination: | 97.2855° |
| perigee height: | 464 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 333.2559° |
| argument of perigee: | 88.3703° |
| revolutions per day: | 15.33451934 |
| mean anomaly at epoch: | 271.7724° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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