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 67892U 26145.36319818 +.00000000 +00000-0 +76460-3 0 00008
2 67892 97.2852 78.9663 0002303 112.9033 247.2453 15.33447555 02
| Epoch (UTC): | 25 May 2026 08:43:00 |
| Eccentricity: | 0.0002303 |
| inclination: | 97.2852° |
| perigee height: | 464 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 78.9663° |
| argument of perigee: | 112.9033° |
| revolutions per day: | 15.33447555 |
| mean anomaly at epoch: | 247.2453° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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