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 58662U 26145.55991294 +.00000000 +00000-0 +27176-3 0 00008
2 58662 97.4476 264.9503 0007890 48.2663 311.9253 15.34605528 01
| Epoch (UTC): | 25 May 2026 13:26:16 |
| Eccentricity: | 0.0007890 |
| inclination: | 97.4476° |
| perigee height: | 457 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 264.9503° |
| argument of perigee: | 48.2663° |
| revolutions per day: | 15.34605528 |
| mean anomaly at epoch: | 311.9253° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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