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 47284U 26145.33227750 +.00000000 +00000-0 +10849-2 0 00009
2 47284 87.8961 355.2100 0001539 86.2071 273.9233 13.12442574 06
| Epoch (UTC): | 25 May 2026 07:58:28 |
| Eccentricity: | 0.0001539 |
| inclination: | 87.8961° |
| perigee height: | 1213 km |
| apogee height: | 1215 km |
| right ascension of ascending node: | 355.2100° |
| argument of perigee: | 86.2071° |
| revolutions per day: | 13.12442574 |
| mean anomaly at epoch: | 273.9233° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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