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 43912U 26145.46727331 +.00000000 +00000-0 +83617-4 0 00002
2 43912 50.0117 23.8752 0015342 266.3167 93.5994 14.29021396 04
| Epoch (UTC): | 25 May 2026 11:12:52 |
| Eccentricity: | 0.0015342 |
| inclination: | 50.0117° |
| perigee height: | 784 km |
| apogee height: | 806 km |
| right ascension of ascending node: | 23.8752° |
| argument of perigee: | 266.3167° |
| revolutions per day: | 14.29021396 |
| mean anomaly at epoch: | 93.5994° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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