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 68031U 26145.42178707 +.00000000 +00000-0 +34943-3 0 00001
2 68031 97.2845 94.4479 0001517 94.0486 266.0930 15.33444010 08
| Epoch (UTC): | 25 May 2026 10:07:22 |
| Eccentricity: | 0.0001517 |
| inclination: | 97.2845° |
| perigee height: | 465 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 94.4479° |
| argument of perigee: | 94.0486° |
| revolutions per day: | 15.33444010 |
| mean anomaly at epoch: | 266.0930° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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