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 56347U 26145.42053080 +.00000000 +00000-0 -42192-3 0 00000
2 56347 97.4483 146.4951 0001902 91.3222 268.8223 15.05686214 02
| Epoch (UTC): | 25 May 2026 10:05:33 |
| Eccentricity: | 0.0001902 |
| inclination: | 97.4483° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 146.4951° |
| argument of perigee: | 91.3222° |
| revolutions per day: | 15.05686214 |
| mean anomaly at epoch: | 268.8223° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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