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 68136U 26145.39151980 +.00000000 +00000-0 +81500-4 0 00009
2 68136 50.0042 137.6581 0000197 355.1185 4.9685 13.29327408 04
| Epoch (UTC): | 25 May 2026 09:23:47 |
| Eccentricity: | 0.0000197 |
| inclination: | 50.0042° |
| perigee height: | 1149 km |
| apogee height: | 1149 km |
| right ascension of ascending node: | 137.6581° |
| argument of perigee: | 355.1185° |
| revolutions per day: | 13.29327408 |
| mean anomaly at epoch: | 4.9685° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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