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 67923U 26145.47735248 +.00000000 +00000-0 +57154-3 0 00003
2 67923 43.0018 171.8072 0001538 275.0941 84.9735 15.27597722 09
| Epoch (UTC): | 25 May 2026 11:27:23 |
| Eccentricity: | 0.0001538 |
| inclination: | 43.0018° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 171.8072° |
| argument of perigee: | 275.0941° |
| revolutions per day: | 15.27597722 |
| mean anomaly at epoch: | 84.9735° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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