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 67639U 26145.06352844 +.00000000 +00000-0 +55012-3 0 00000
2 67639 43.0057 68.4798 0002889 275.8918 84.1604 15.27594507 09
| Epoch (UTC): | 25 May 2026 01:31:28 |
| Eccentricity: | 0.0002889 |
| inclination: | 43.0057° |
| perigee height: | 481 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 68.4798° |
| argument of perigee: | 275.8918° |
| revolutions per day: | 15.27594507 |
| mean anomaly at epoch: | 84.1604° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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