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 56378U 26145.39597294 +.00000000 +00000-0 +36929-4 0 00001
2 56378 43.0043 124.4640 0001576 284.5174 75.5503 15.27579358 03
| Epoch (UTC): | 25 May 2026 09:30:12 |
| Eccentricity: | 0.0001576 |
| inclination: | 43.0043° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 124.4640° |
| argument of perigee: | 284.5174° |
| revolutions per day: | 15.27579358 |
| mean anomaly at epoch: | 75.5503° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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