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 43023U 26145.61184933 +.00000000 +00000-0 +23846-3 0 00004
2 43023 97.4840 251.4704 0003960 318.9451 41.1493 15.33472445 08
| Epoch (UTC): | 25 May 2026 14:41:03 |
| Eccentricity: | 0.0003960 |
| inclination: | 97.4840° |
| perigee height: | 463 km |
| apogee height: | 468 km |
| right ascension of ascending node: | 251.4704° |
| argument of perigee: | 318.9451° |
| revolutions per day: | 15.33472445 |
| mean anomaly at epoch: | 41.1493° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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