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 68132U 26145.34971889 +.00000000 +00000-0 +86024-4 0 00004
2 68132 50.0025 138.0885 0000277 12.4057 347.6822 13.29330444 07
| Epoch (UTC): | 25 May 2026 08:23:35 |
| Eccentricity: | 0.0000277 |
| inclination: | 50.0025° |
| perigee height: | 1149 km |
| apogee height: | 1149 km |
| right ascension of ascending node: | 138.0885° |
| argument of perigee: | 12.4057° |
| revolutions per day: | 13.29330444 |
| mean anomaly at epoch: | 347.6822° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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