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 56143U 26145.51670922 +.00000000 +00000-0 +45871-3 0 00000
2 56143 42.9994 80.4529 0000987 225.7006 134.3761 15.16060045 05
| Epoch (UTC): | 25 May 2026 12:24:03 |
| Eccentricity: | 0.0000987 |
| inclination: | 42.9994° |
| perigee height: | 517 km |
| apogee height: | 518 km |
| right ascension of ascending node: | 80.4529° |
| argument of perigee: | 225.7006° |
| revolutions per day: | 15.16060045 |
| mean anomaly at epoch: | 134.3761° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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