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 58885U 26143.95066933 +.00000000 +00000-0 +30199-4 0 00000
2 58885 53.1613 332.8491 0001094 85.5653 274.5473 15.31704434 05
| Epoch (UTC): | 23 May 2026 22:48:57 |
| Eccentricity: | 0.0001094 |
| inclination: | 53.1613° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 332.8491° |
| argument of perigee: | 85.5653° |
| revolutions per day: | 15.31704434 |
| mean anomaly at epoch: | 274.5473° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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