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 67819U 26145.05324646 +.00000000 +00000-0 +34723-3 0 00004
2 67819 97.2851 333.1494 0001573 95.6775 264.4647 15.33456479 07
| Epoch (UTC): | 25 May 2026 01:16:40 |
| Eccentricity: | 0.0001573 |
| inclination: | 97.2851° |
| perigee height: | 464 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 333.1494° |
| argument of perigee: | 95.6775° |
| revolutions per day: | 15.33456479 |
| mean anomaly at epoch: | 264.4647° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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