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 67792U 26145.41276860 +.00000000 +00000-0 +23009-3 0 00003
2 67792 51.9000 223.5205 0004038 5.9511 354.1497 14.76348195 04
| Epoch (UTC): | 25 May 2026 09:54:23 |
| Eccentricity: | 0.0004038 |
| inclination: | 51.9000° |
| perigee height: | 638 km |
| apogee height: | 644 km |
| right ascension of ascending node: | 223.5205° |
| argument of perigee: | 5.9511° |
| revolutions per day: | 14.76348195 |
| mean anomaly at epoch: | 354.1497° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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