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 47862U 26145.56581995 +.00000000 +00000-0 +13452-2 0 00003
2 47862 53.1574 253.4542 0004838 346.2052 13.8825 15.50657294 05
| Epoch (UTC): | 25 May 2026 13:34:46 |
| Eccentricity: | 0.0004838 |
| inclination: | 53.1574° |
| perigee height: | 412 km |
| apogee height: | 418 km |
| right ascension of ascending node: | 253.4542° |
| argument of perigee: | 346.2052° |
| revolutions per day: | 15.50657294 |
| mean anomaly at epoch: | 13.8825° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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