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 68734U 26145.58335647 +.00000000 +00000-0 -17351-1 0 00009
2 68734 97.2853 9.2980 0000882 136.4532 340.5444 15.49726025 09
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0000882 |
| inclination: | 97.2853° |
| perigee height: | 417 km |
| apogee height: | 418 km |
| right ascension of ascending node: | 9.2980° |
| argument of perigee: | 136.4532° |
| revolutions per day: | 15.49726025 |
| mean anomaly at epoch: | 340.5444° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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