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 67332U 26145.57766597 +.00000000 +00000-0 +43864-3 0 00002
2 67332 42.9991 251.4131 0001232 276.1442 83.9269 15.27597047 02
| Epoch (UTC): | 25 May 2026 13:51:50 |
| Eccentricity: | 0.0001232 |
| inclination: | 42.9991° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 251.4131° |
| argument of perigee: | 276.1442° |
| revolutions per day: | 15.27597047 |
| mean anomaly at epoch: | 83.9269° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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