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 67343U 26145.50647912 +.00000000 +00000-0 +54861-3 0 00005
2 67343 43.0015 153.1066 0001728 271.6390 88.4264 15.27590532 07
| Epoch (UTC): | 25 May 2026 12:09:19 |
| Eccentricity: | 0.0001728 |
| inclination: | 43.0015° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 153.1066° |
| argument of perigee: | 271.6390° |
| revolutions per day: | 15.27590532 |
| mean anomaly at epoch: | 88.4264° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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