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 67032U 26145.52620311 +.00000000 +00000-0 +66682-3 0 00000
2 67032 43.0002 323.8654 0000797 283.2157 76.8605 15.27592206 02
| Epoch (UTC): | 25 May 2026 12:37:43 |
| Eccentricity: | 0.0000797 |
| inclination: | 43.0002° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 323.8654° |
| argument of perigee: | 283.2157° |
| revolutions per day: | 15.27592206 |
| mean anomaly at epoch: | 76.8605° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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