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 47288U 26145.28498000 +.00000000 +00000-0 -33845-4 0 00009
2 47288 87.8953 355.2245 0001707 99.8175 260.3146 13.12440475 04
| Epoch (UTC): | 25 May 2026 06:50:22 |
| Eccentricity: | 0.0001707 |
| inclination: | 87.8953° |
| perigee height: | 1212 km |
| apogee height: | 1215 km |
| right ascension of ascending node: | 355.2245° |
| argument of perigee: | 99.8175° |
| revolutions per day: | 13.12440475 |
| mean anomaly at epoch: | 260.3146° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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