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 68404U 26145.65114132 +.00000000 +00000-0 +41014-3 0 00009
2 68404 97.2853 288.2670 0001636 90.3798 269.7632 15.33460356 04
| Epoch (UTC): | 25 May 2026 15:37:38 |
| Eccentricity: | 0.0001636 |
| inclination: | 97.2853° |
| perigee height: | 464 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 288.2670° |
| argument of perigee: | 90.3798° |
| revolutions per day: | 15.33460356 |
| mean anomaly at epoch: | 269.7632° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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