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 43914U 26145.48194220 +.00000000 +00000-0 +78241-4 0 00008
2 43914 50.0091 320.5246 0006693 186.9247 173.1540 13.43819404 09
| Epoch (UTC): | 25 May 2026 11:33:59 |
| Eccentricity: | 0.0006693 |
| inclination: | 50.0091° |
| perigee height: | 1090 km |
| apogee height: | 1100 km |
| right ascension of ascending node: | 320.5246° |
| argument of perigee: | 186.9247° |
| revolutions per day: | 13.43819404 |
| mean anomaly at epoch: | 173.1540° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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