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 58895U 26144.91541711 +.00000000 +00000-0 +13091-4 0 00002
2 58895 53.1610 328.2135 0001705 95.8836 264.2360 15.31708234 06
| Epoch (UTC): | 24 May 2026 21:58:12 |
| Eccentricity: | 0.0001705 |
| inclination: | 53.1610° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 328.2135° |
| argument of perigee: | 95.8836° |
| revolutions per day: | 15.31708234 |
| mean anomaly at epoch: | 264.2360° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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