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 56349U 26144.96230286 +.00000000 +00000-0 +74288-5 0 00007
2 56349 97.4485 144.9708 0002122 66.7223 293.4228 15.05658747 00
| Epoch (UTC): | 24 May 2026 23:05:42 |
| Eccentricity: | 0.0002122 |
| inclination: | 97.4485° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 144.9708° |
| argument of perigee: | 66.7223° |
| revolutions per day: | 15.05658747 |
| mean anomaly at epoch: | 293.4228° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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