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 47486U 26145.48128707 +.00000000 +00000-0 +17301-3 0 00002
2 47486 97.2274 187.0941 0004666 280.5618 79.5098 15.31879099 04
| Epoch (UTC): | 25 May 2026 11:33:03 |
| Eccentricity: | 0.0004666 |
| inclination: | 97.2274° |
| perigee height: | 467 km |
| apogee height: | 473 km |
| right ascension of ascending node: | 187.0941° |
| argument of perigee: | 280.5618° |
| revolutions per day: | 15.31879099 |
| mean anomaly at epoch: | 79.5098° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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