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 68385U 26145.35749740 +.00000000 +00000-0 +70390-3 0 00002
2 68385 97.2851 287.9002 0001312 67.8328 292.3054 15.33452601 08
| Epoch (UTC): | 25 May 2026 08:34:47 |
| Eccentricity: | 0.0001312 |
| inclination: | 97.2851° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 287.9002° |
| argument of perigee: | 67.8328° |
| revolutions per day: | 15.33452601 |
| mean anomaly at epoch: | 292.3054° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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