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 67687U 26145.12106645 +.00000000 +00000-0 +63782-3 0 00009
2 67687 51.6302 50.0450 0009759 97.5806 262.6296 15.58388834 08
| Epoch (UTC): | 25 May 2026 02:54:20 |
| Eccentricity: | 0.0009759 |
| inclination: | 51.6302° |
| perigee height: | 386 km |
| apogee height: | 399 km |
| right ascension of ascending node: | 50.0450° |
| argument of perigee: | 97.5806° |
| revolutions per day: | 15.58388834 |
| mean anomaly at epoch: | 262.6296° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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