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 67593U 26145.60018105 +.00000000 +00000-0 +12064-3 0 00008
2 67593 97.2852 210.7624 0000423 82.2392 277.8899 15.33440254 03
| Epoch (UTC): | 25 May 2026 14:24:15 |
| Eccentricity: | 0.0000423 |
| inclination: | 97.2852° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 210.7624° |
| argument of perigee: | 82.2392° |
| revolutions per day: | 15.33440254 |
| mean anomaly at epoch: | 277.8899° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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