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 43001U 26143.96999845 +.00000000 +00000-0 +00000-0 0 00006
2 43001 56.6723 63.8816 0011367 323.2032 36.7137 1.86231088 08
| Epoch (UTC): | 23 May 2026 23:16:47 |
| Eccentricity: | 0.0011367 |
| inclination: | 56.6723° |
| perigee height: | 21496 km |
| apogee height: | 21560 km |
| right ascension of ascending node: | 63.8816° |
| argument of perigee: | 323.2032° |
| revolutions per day: | 1.86231088 |
| mean anomaly at epoch: | 36.7137° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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