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 67665U 26145.52231389 +.00000000 +00000-0 +44366-3 0 00000
2 67665 97.2846 178.7134 0000799 81.6917 278.4417 15.33469323 08
| Epoch (UTC): | 25 May 2026 12:32:07 |
| Eccentricity: | 0.0000799 |
| inclination: | 97.2846° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 178.7134° |
| argument of perigee: | 81.6917° |
| revolutions per day: | 15.33469323 |
| mean anomaly at epoch: | 278.4417° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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