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 56290U 26145.34854006 +.00000000 +00000-0 +14924-3 0 00006
2 56290 43.0026 136.0183 0001202 272.4969 87.5746 15.27569918 05
| Epoch (UTC): | 25 May 2026 08:21:53 |
| Eccentricity: | 0.0001202 |
| inclination: | 43.0026° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 136.0183° |
| argument of perigee: | 272.4969° |
| revolutions per day: | 15.27569918 |
| mean anomaly at epoch: | 87.5746° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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