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 47376U 26145.51316192 +.00000000 +00000-0 -81170-4 0 00008
2 47376 53.1605 65.2204 0001340 88.8245 271.2910 15.31694397 01
| Epoch (UTC): | 25 May 2026 12:18:57 |
| Eccentricity: | 0.0001340 |
| inclination: | 53.1605° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 65.2204° |
| argument of perigee: | 88.8245° |
| revolutions per day: | 15.31694397 |
| mean anomaly at epoch: | 271.2910° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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