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 47290U 26145.34244022 +.00000000 +00000-0 +12851-2 0 00003
2 47290 87.8964 355.1836 0001486 93.3256 266.8043 13.12441281 00
| Epoch (UTC): | 25 May 2026 08:13:06 |
| Eccentricity: | 0.0001486 |
| inclination: | 87.8964° |
| perigee height: | 1213 km |
| apogee height: | 1215 km |
| right ascension of ascending node: | 355.1836° |
| argument of perigee: | 93.3256° |
| revolutions per day: | 13.12441281 |
| mean anomaly at epoch: | 266.8043° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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