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 68131U 26145.43325494 +.00000000 +00000-0 +84062-4 0 00008
2 68131 49.9980 137.8313 0000205 355.1602 4.9268 13.29329729 01
| Epoch (UTC): | 25 May 2026 10:23:53 |
| Eccentricity: | 0.0000205 |
| inclination: | 49.9980° |
| perigee height: | 1149 km |
| apogee height: | 1149 km |
| right ascension of ascending node: | 137.8313° |
| argument of perigee: | 355.1602° |
| revolutions per day: | 13.29329729 |
| mean anomaly at epoch: | 4.9268° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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