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 68400U 26145.34661917 +.00000000 +00000-0 +68791-3 0 00000
2 68400 97.2841 287.9145 0001582 79.7371 280.4050 15.33462660 02
| Epoch (UTC): | 25 May 2026 08:19:07 |
| Eccentricity: | 0.0001582 |
| inclination: | 97.2841° |
| perigee height: | 464 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 287.9145° |
| argument of perigee: | 79.7371° |
| revolutions per day: | 15.33462660 |
| mean anomaly at epoch: | 280.4050° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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