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 56144U 26145.07412576 +.00000000 +00000-0 +16680-4 0 00008
2 56144 43.0032 75.4726 0001746 274.0350 86.0302 15.27577096 02
| Epoch (UTC): | 25 May 2026 01:46:44 |
| Eccentricity: | 0.0001746 |
| inclination: | 43.0032° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 75.4726° |
| argument of perigee: | 274.0350° |
| revolutions per day: | 15.27577096 |
| mean anomaly at epoch: | 86.0302° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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