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 56384U 26145.62169014 +.00000000 +00000-0 +17059-4 0 00002
2 56384 43.0031 123.5746 0001331 266.4503 93.6196 15.27576671 02
| Epoch (UTC): | 25 May 2026 14:55:14 |
| Eccentricity: | 0.0001331 |
| inclination: | 43.0031° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 123.5746° |
| argument of perigee: | 266.4503° |
| revolutions per day: | 15.27576671 |
| mean anomaly at epoch: | 93.6196° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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