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 47264U 26145.53725110 +.00000000 +00000-0 -10281-2 0 00003
2 47264 87.8959 355.1568 0001926 95.8562 264.2786 13.12441800 06
| Epoch (UTC): | 25 May 2026 12:53:38 |
| Eccentricity: | 0.0001926 |
| inclination: | 87.8959° |
| perigee height: | 1212 km |
| apogee height: | 1215 km |
| right ascension of ascending node: | 355.1568° |
| argument of perigee: | 95.8562° |
| revolutions per day: | 13.12441800 |
| mean anomaly at epoch: | 264.2786° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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