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 68401U 26145.37108980 +.00000000 +00000-0 +46817-3 0 00005
2 68401 97.2852 287.8822 0001453 54.5909 305.5469 15.33455470 05
| Epoch (UTC): | 25 May 2026 08:54:22 |
| Eccentricity: | 0.0001453 |
| inclination: | 97.2852° |
| perigee height: | 465 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 287.8822° |
| argument of perigee: | 54.5909° |
| revolutions per day: | 15.33455470 |
| mean anomaly at epoch: | 305.5469° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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