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 43339U 26143.32889131 +.00000000 +00000-0 +00000-0 0 00006
2 43339 0.0094 309.1271 0000117 90.3436 93.9667 1.00271058 08
| Epoch (UTC): | 23 May 2026 07:53:36 |
| Eccentricity: | 0.0000117 |
| inclination: | 0.0094° |
| perigee height: | 35786 km |
| apogee height: | 35787 km |
| right ascension of ascending node: | 309.1271° |
| argument of perigee: | 90.3436° |
| revolutions per day: | 1.00271058 |
| mean anomaly at epoch: | 93.9667° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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