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 47883U 26144.75356900 +.00000000 +00000-0 +10457-2 0 00004
2 47883 53.1559 263.7009 0004396 291.2238 68.8305 15.56064717 08
| Epoch (UTC): | 24 May 2026 18:05:08 |
| Eccentricity: | 0.0004396 |
| inclination: | 53.1559° |
| perigee height: | 396 km |
| apogee height: | 402 km |
| right ascension of ascending node: | 263.7009° |
| argument of perigee: | 291.2238° |
| revolutions per day: | 15.56064717 |
| mean anomaly at epoch: | 68.8305° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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