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 58152U 26145.66668980 +.00000000 +00000-0 +19227-2 0 00004
2 58152 53.1601 222.3065 0001318 75.5620 196.7417 15.31670584 02
| Epoch (UTC): | 25 May 2026 16:00:01 |
| Eccentricity: | 0.0001318 |
| inclination: | 53.1601° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 222.3065° |
| argument of perigee: | 75.5620° |
| revolutions per day: | 15.31670584 |
| mean anomaly at epoch: | 196.7417° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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