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 47404U 26145.66668980 +.00000000 +00000-0 +44125-4 0 00009
2 47404 53.0431 355.8449 0003529 130.6753 130.8920 15.78509879 01
| Epoch (UTC): | 25 May 2026 16:00:01 |
| Eccentricity: | 0.0003529 |
| inclination: | 53.0431° |
| perigee height: | 332 km |
| apogee height: | 337 km |
| right ascension of ascending node: | 355.8449° |
| argument of perigee: | 130.6753° |
| revolutions per day: | 15.78509879 |
| mean anomaly at epoch: | 130.8920° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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