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 43002U 26144.98259096 +.00000000 +00000-0 +00000-0 0 00007
2 43002 56.6725 63.8844 0009764 345.7840 14.1813 1.86230543 02
| Epoch (UTC): | 24 May 2026 23:34:55 |
| Eccentricity: | 0.0009764 |
| inclination: | 56.6725° |
| perigee height: | 21501 km |
| apogee height: | 21555 km |
| right ascension of ascending node: | 63.8844° |
| argument of perigee: | 345.7840° |
| revolutions per day: | 1.86230543 |
| mean anomaly at epoch: | 14.1813° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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