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 47373U 26145.48053407 +.00000000 +00000-0 +20394-3 0 00007
2 47373 53.1604 65.3335 0001202 83.8192 276.2946 15.31705456 09
| Epoch (UTC): | 25 May 2026 11:31:58 |
| Eccentricity: | 0.0001202 |
| inclination: | 53.1604° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 65.3335° |
| argument of perigee: | 83.8192° |
| revolutions per day: | 15.31705456 |
| mean anomaly at epoch: | 276.2946° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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