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 58503U 26145.55324764 +.00000000 +00000-0 +85285-3 0 00009
2 58503 97.3843 184.3594 0007081 220.1543 139.9212 16.00136173 09
| Epoch (UTC): | 25 May 2026 13:16:40 |
| Eccentricity: | 0.0007081 |
| inclination: | 97.3843° |
| perigee height: | 269 km |
| apogee height: | 279 km |
| right ascension of ascending node: | 184.3594° |
| argument of perigee: | 220.1543° |
| revolutions per day: | 16.00136173 |
| mean anomaly at epoch: | 139.9212° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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