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 58882U 26145.50003470 +.00000000 +00000-0 +98638-3 0 00008
2 58882 53.1600 325.2901 0001216 96.2792 353.5202 15.34375641 04
| Epoch (UTC): | 25 May 2026 12:00:02 |
| Eccentricity: | 0.0001216 |
| inclination: | 53.1600° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 325.2901° |
| argument of perigee: | 96.2792° |
| revolutions per day: | 15.34375641 |
| mean anomaly at epoch: | 353.5202° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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