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 67743U 26145.12120317 +.00000000 +00000-0 +45255-3 0 00009
2 67743 97.2851 198.7134 0000645 111.5286 248.6026 15.33461026 02
| Epoch (UTC): | 25 May 2026 02:54:31 |
| Eccentricity: | 0.0000645 |
| inclination: | 97.2851° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 198.7134° |
| argument of perigee: | 111.5286° |
| revolutions per day: | 15.33461026 |
| mean anomaly at epoch: | 248.6026° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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