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 67327U 26145.59037014 +.00000000 +00000-0 +92428-3 0 00003
2 67327 43.0007 250.6406 0001498 276.5169 83.5512 15.27600541 07
| Epoch (UTC): | 25 May 2026 14:10:07 |
| Eccentricity: | 0.0001498 |
| inclination: | 43.0007° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 250.6406° |
| argument of perigee: | 276.5169° |
| revolutions per day: | 15.27600541 |
| mean anomaly at epoch: | 83.5512° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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