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 67799U 26145.47468573 +.00000000 +00000-0 +47405-3 0 00006
2 67799 97.2854 333.4931 0001895 96.9854 263.1604 15.33457022 09
| Epoch (UTC): | 25 May 2026 11:23:32 |
| Eccentricity: | 0.0001895 |
| inclination: | 97.2854° |
| perigee height: | 464 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 333.4931° |
| argument of perigee: | 96.9854° |
| revolutions per day: | 15.33457022 |
| mean anomaly at epoch: | 263.1604° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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