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 47546U 26145.62386080 +.00000000 +00000-0 +18712-4 0 00003
2 47546 67.1513 39.9375 0005694 263.9747 96.0689 13.97020305 07
| Epoch (UTC): | 25 May 2026 14:58:21 |
| Eccentricity: | 0.0005694 |
| inclination: | 67.1513° |
| perigee height: | 900 km |
| apogee height: | 908 km |
| right ascension of ascending node: | 39.9375° |
| argument of perigee: | 263.9747° |
| revolutions per day: | 13.97020305 |
| mean anomaly at epoch: | 96.0689° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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