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 67342U 26145.36029078 +.00000000 +00000-0 +54826-3 0 00006
2 67342 43.0011 153.7266 0001611 277.5090 82.5579 15.27588707 08
| Epoch (UTC): | 25 May 2026 08:38:49 |
| Eccentricity: | 0.0001611 |
| inclination: | 43.0011° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 153.7266° |
| argument of perigee: | 277.5090° |
| revolutions per day: | 15.27588707 |
| mean anomaly at epoch: | 82.5579° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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