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 56006U 26145.66668980 +.00000000 +00000-0 +14403-2 0 00001
2 56006 43.0005 352.1951 0001279 279.9262 175.8115 15.21233347 02
| Epoch (UTC): | 25 May 2026 16:00:01 |
| Eccentricity: | 0.0001279 |
| inclination: | 43.0005° |
| perigee height: | 501 km |
| apogee height: | 503 km |
| right ascension of ascending node: | 352.1951° |
| argument of perigee: | 279.9262° |
| revolutions per day: | 15.21233347 |
| mean anomaly at epoch: | 175.8115° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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