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 58821U 26145.63199483 +.00000000 +00000-0 +86754-3 0 00001
2 58821 97.4465 241.1469 0005503 156.5012 203.6501 15.68099792 04
| Epoch (UTC): | 25 May 2026 15:10:04 |
| Eccentricity: | 0.0005503 |
| inclination: | 97.4465° |
| perigee height: | 361 km |
| apogee height: | 368 km |
| right ascension of ascending node: | 241.1469° |
| argument of perigee: | 156.5012° |
| revolutions per day: | 15.68099792 |
| mean anomaly at epoch: | 203.6501° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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