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 67313U 26145.64048625 +.00000000 +00000-0 +58274-3 0 00005
2 67313 42.9991 251.0325 0001407 279.9794 80.0899 15.27594011 02
| Epoch (UTC): | 25 May 2026 15:22:18 |
| Eccentricity: | 0.0001407 |
| inclination: | 42.9991° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 251.0325° |
| argument of perigee: | 279.9794° |
| revolutions per day: | 15.27594011 |
| mean anomaly at epoch: | 80.0899° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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