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 47273U 26145.28991602 +.00000000 +00000-0 -61539-3 0 00009
2 47273 87.8947 355.2252 0001686 88.5396 271.5926 13.12441280 00
| Epoch (UTC): | 25 May 2026 06:57:28 |
| Eccentricity: | 0.0001686 |
| inclination: | 87.8947° |
| perigee height: | 1212 km |
| apogee height: | 1215 km |
| right ascension of ascending node: | 355.2252° |
| argument of perigee: | 88.5396° |
| revolutions per day: | 13.12441280 |
| mean anomaly at epoch: | 271.5926° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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