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 56178U 26145.62815427 +.00000000 +00000-0 +48979-4 0 00004
2 56178 98.1247 50.6939 0008405 237.7631 122.2759 14.65830576 01
| Epoch (UTC): | 25 May 2026 15:04:32 |
| Eccentricity: | 0.0008405 |
| inclination: | 98.1247° |
| perigee height: | 668 km |
| apogee height: | 680 km |
| right ascension of ascending node: | 50.6939° |
| argument of perigee: | 237.7631° |
| revolutions per day: | 14.65830576 |
| mean anomaly at epoch: | 122.2759° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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