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 67097U 26145.52639193 +.00000000 +00000-0 +96040-3 0 00000
2 67097 70.0013 180.8426 0003733 267.4545 92.6187 14.98368173 03
| Epoch (UTC): | 25 May 2026 12:38:00 |
| Eccentricity: | 0.0003733 |
| inclination: | 70.0013° |
| perigee height: | 569 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 180.8426° |
| argument of perigee: | 267.4545° |
| revolutions per day: | 14.98368173 |
| mean anomaly at epoch: | 92.6187° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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