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 47272U 26145.55265161 +.00000000 +00000-0 +29933-3 0 00003
2 47272 87.8954 355.1728 0001690 89.5110 270.6212 13.12444288 03
| Epoch (UTC): | 25 May 2026 13:15:49 |
| Eccentricity: | 0.0001690 |
| inclination: | 87.8954° |
| perigee height: | 1212 km |
| apogee height: | 1215 km |
| right ascension of ascending node: | 355.1728° |
| argument of perigee: | 89.5110° |
| revolutions per day: | 13.12444288 |
| mean anomaly at epoch: | 270.6212° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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