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 68343U 26145.26969683 +.00000000 +00000-0 +88001-3 0 00004
2 68343 53.1595 348.7586 0001936 83.1592 276.9631 15.34406008 07
| Epoch (UTC): | 25 May 2026 06:28:21 |
| Eccentricity: | 0.0001936 |
| inclination: | 53.1595° |
| perigee height: | 461 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 348.7586° |
| argument of perigee: | 83.1592° |
| revolutions per day: | 15.34406008 |
| mean anomaly at epoch: | 276.9631° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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