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 67123U 26145.55349406 +.00000000 +00000-0 +32269-3 0 00001
2 67123 42.9992 94.7193 0000477 284.3767 75.7031 15.27584384 04
| Epoch (UTC): | 25 May 2026 13:17:01 |
| Eccentricity: | 0.0000477 |
| inclination: | 42.9992° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 94.7193° |
| argument of perigee: | 284.3767° |
| revolutions per day: | 15.27584384 |
| mean anomaly at epoch: | 75.7031° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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