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 67625U 26145.06481568 +.00000000 +00000-0 +13433-2 0 00001
2 67625 43.0008 68.5046 0000649 233.0147 127.0645 15.27615924 08
| Epoch (UTC): | 25 May 2026 01:33:20 |
| Eccentricity: | 0.0000649 |
| inclination: | 43.0008° |
| perigee height: | 482 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 68.5046° |
| argument of perigee: | 233.0147° |
| revolutions per day: | 15.27615924 |
| mean anomaly at epoch: | 127.0645° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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