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 47260U 26145.29838792 +.00000000 +00000-0 -97184-3 0 00001
2 47260 87.8959 355.1943 0001712 77.8077 282.3244 13.12442785 06
| Epoch (UTC): | 25 May 2026 07:09:40 |
| Eccentricity: | 0.0001712 |
| inclination: | 87.8959° |
| perigee height: | 1212 km |
| apogee height: | 1215 km |
| right ascension of ascending node: | 355.1943° |
| argument of perigee: | 77.8077° |
| revolutions per day: | 13.12442785 |
| mean anomaly at epoch: | 282.3244° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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