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 56350U 26145.47869501 +.00000000 +00000-0 -36655-5 0 00001
2 56350 97.4448 146.5702 0001818 95.5708 264.5727 15.05653894 03
| Epoch (UTC): | 25 May 2026 11:29:19 |
| Eccentricity: | 0.0001818 |
| inclination: | 97.4448° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 146.5702° |
| argument of perigee: | 95.5708° |
| revolutions per day: | 15.05653894 |
| mean anomaly at epoch: | 264.5727° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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