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 43080U 26145.60509962 +.00000000 +00000-0 +29993-3 0 00008
2 43080 97.1208 186.4603 0001592 25.5937 334.5381 15.25994690 07
| Epoch (UTC): | 25 May 2026 14:31:20 |
| Eccentricity: | 0.0001592 |
| inclination: | 97.1208° |
| perigee height: | 487 km |
| apogee height: | 489 km |
| right ascension of ascending node: | 186.4603° |
| argument of perigee: | 25.5937° |
| revolutions per day: | 15.25994690 |
| mean anomaly at epoch: | 334.5381° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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