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 47357U 26145.66668980 +.00000000 +00000-0 +20163-2 0 00000
2 47357 53.1594 64.8552 0001099 100.2938 281.9047 15.31664682 00
| Epoch (UTC): | 25 May 2026 16:00:01 |
| Eccentricity: | 0.0001099 |
| inclination: | 53.1594° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 64.8552° |
| argument of perigee: | 100.2938° |
| revolutions per day: | 15.31664682 |
| mean anomaly at epoch: | 281.9047° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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