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 67292U 26145.63945111 +.00000000 +00000-0 +38502-3 0 00008
2 67292 97.3942 220.9933 0010477 79.8889 280.3530 15.24510445 00
| Epoch (UTC): | 25 May 2026 15:20:48 |
| Eccentricity: | 0.0010477 |
| inclination: | 97.3942° |
| perigee height: | 485 km |
| apogee height: | 499 km |
| right ascension of ascending node: | 220.9933° |
| argument of perigee: | 79.8889° |
| revolutions per day: | 15.24510445 |
| mean anomaly at epoch: | 280.3530° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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