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 67556U 26145.34638124 +.00000000 +00000-0 +76609-4 0 00003
2 67556 88.9987 270.8517 0004791 127.0667 233.0924 13.52692423 00
| Epoch (UTC): | 25 May 2026 08:18:47 |
| Eccentricity: | 0.0004791 |
| inclination: | 88.9987° |
| perigee height: | 1059 km |
| apogee height: | 1066 km |
| right ascension of ascending node: | 270.8517° |
| argument of perigee: | 127.0667° |
| revolutions per day: | 13.52692423 |
| mean anomaly at epoch: | 233.0924° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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