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 56002U 26145.60295128 +.00000000 +00000-0 +12356-4 0 00008
2 56002 43.0060 345.1218 0001578 265.5385 94.5287 15.27574920 04
| Epoch (UTC): | 25 May 2026 14:28:14 |
| Eccentricity: | 0.0001578 |
| inclination: | 43.0060° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 345.1218° |
| argument of perigee: | 265.5385° |
| revolutions per day: | 15.27574920 |
| mean anomaly at epoch: | 94.5287° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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