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 68813U 26145.11225839 +.00000000 +00000-0 +11885-2 0 00003
2 68813 97.2839 351.7648 0001504 83.3303 276.8133 15.75245184 02
| Epoch (UTC): | 25 May 2026 02:41:39 |
| Eccentricity: | 0.0001504 |
| inclination: | 97.2839° |
| perigee height: | 343 km |
| apogee height: | 345 km |
| right ascension of ascending node: | 351.7648° |
| argument of perigee: | 83.3303° |
| revolutions per day: | 15.75245184 |
| mean anomaly at epoch: | 276.8133° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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