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 67398U 26144.93585574 +.00000000 +00000-0 +17937-3 0 00009
2 67398 97.4561 144.4452 0008540 74.5494 285.6684 15.18931079 04
| Epoch (UTC): | 24 May 2026 22:27:37 |
| Eccentricity: | 0.0008540 |
| inclination: | 97.4561° |
| perigee height: | 503 km |
| apogee height: | 515 km |
| right ascension of ascending node: | 144.4452° |
| argument of perigee: | 74.5494° |
| revolutions per day: | 15.18931079 |
| mean anomaly at epoch: | 285.6684° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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