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 56339U 26144.95398536 +.00000000 +00000-0 -11847-3 0 00009
2 56339 97.4509 144.9774 0002087 108.2207 251.9247 15.05657606 06
| Epoch (UTC): | 24 May 2026 22:53:44 |
| Eccentricity: | 0.0002087 |
| inclination: | 97.4509° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 144.9774° |
| argument of perigee: | 108.2207° |
| revolutions per day: | 15.05657606 |
| mean anomaly at epoch: | 251.9247° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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