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 47676U 26145.66668980 +.00000000 +00000-0 +47122-3 0 00009
2 47676 53.0437 263.0765 0005233 322.6846 47.0789 15.74773089 03
| Epoch (UTC): | 25 May 2026 16:00:01 |
| Eccentricity: | 0.0005233 |
| inclination: | 53.0437° |
| perigee height: | 342 km |
| apogee height: | 349 km |
| right ascension of ascending node: | 263.0765° |
| argument of perigee: | 322.6846° |
| revolutions per day: | 15.74773089 |
| mean anomaly at epoch: | 47.0789° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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