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 43913U 26145.56391431 +.00000000 +00000-0 +84273-4 0 00001
2 43913 50.0070 262.7800 0005055 283.0084 77.0266 14.29001053 02
| Epoch (UTC): | 25 May 2026 13:32:02 |
| Eccentricity: | 0.0005055 |
| inclination: | 50.0070° |
| perigee height: | 791 km |
| apogee height: | 799 km |
| right ascension of ascending node: | 262.7800° |
| argument of perigee: | 283.0084° |
| revolutions per day: | 14.29001053 |
| mean anomaly at epoch: | 77.0266° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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