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 47382U 26145.37879498 +.00000000 +00000-0 +12083-3 0 00007
2 47382 53.1582 29.8566 0000806 67.1752 292.9334 15.31703555 05
| Epoch (UTC): | 25 May 2026 09:05:27 |
| Eccentricity: | 0.0000806 |
| inclination: | 53.1582° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 29.8566° |
| argument of perigee: | 67.1752° |
| revolutions per day: | 15.31703555 |
| mean anomaly at epoch: | 292.9334° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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