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 47752U 26145.43508076 +.00000000 +00000-0 +10189-2 0 00000
2 47752 53.1552 197.9658 0005562 11.1247 348.9888 15.57218083 05
| Epoch (UTC): | 25 May 2026 10:26:30 |
| Eccentricity: | 0.0005562 |
| inclination: | 53.1552° |
| perigee height: | 392 km |
| apogee height: | 399 km |
| right ascension of ascending node: | 197.9658° |
| argument of perigee: | 11.1247° |
| revolutions per day: | 15.57218083 |
| mean anomaly at epoch: | 348.9888° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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