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 47383U 26145.61715403 +.00000000 +00000-0 +12140-2 0 00003
2 47383 53.1605 16.3610 0001094 159.9210 200.1836 15.32762477 09
| Epoch (UTC): | 25 May 2026 14:48:42 |
| Eccentricity: | 0.0001094 |
| inclination: | 53.1605° |
| perigee height: | 467 km |
| apogee height: | 468 km |
| right ascension of ascending node: | 16.3610° |
| argument of perigee: | 159.9210° |
| revolutions per day: | 15.32762477 |
| mean anomaly at epoch: | 200.1836° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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