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 43619U 26145.58389368 +.00000000 +00000-0 +17933-4 0 00001
2 43619 97.5093 18.8274 0001637 101.2398 258.9008 14.96213728 04
| Epoch (UTC): | 25 May 2026 14:00:48 |
| Eccentricity: | 0.0001637 |
| inclination: | 97.5093° |
| perigee height: | 577 km |
| apogee height: | 580 km |
| right ascension of ascending node: | 18.8274° |
| argument of perigee: | 101.2398° |
| revolutions per day: | 14.96213728 |
| mean anomaly at epoch: | 258.9008° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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