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 47627U 26145.19812418 +.00000000 +00000-0 +11940-2 0 00008
2 47627 53.0480 315.4567 0002980 166.5288 193.5804 15.60006537 07
| Epoch (UTC): | 25 May 2026 04:45:17 |
| Eccentricity: | 0.0002980 |
| inclination: | 53.0480° |
| perigee height: | 386 km |
| apogee height: | 390 km |
| right ascension of ascending node: | 315.4567° |
| argument of perigee: | 166.5288° |
| revolutions per day: | 15.60006537 |
| mean anomaly at epoch: | 193.5804° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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