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 56348U 26145.01488537 +.00000000 +00000-0 -11848-2 0 00008
2 56348 97.4469 144.8951 0002261 82.8449 277.3035 15.05734445 00
| Epoch (UTC): | 25 May 2026 00:21:26 |
| Eccentricity: | 0.0002261 |
| inclination: | 97.4469° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 144.8951° |
| argument of perigee: | 82.8449° |
| revolutions per day: | 15.05734445 |
| mean anomaly at epoch: | 277.3035° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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