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 48470U 26145.42363720 +.00000000 +00000-0 -12205-3 0 00005
2 48470 53.1580 194.1479 0001220 90.1537 269.9604 15.31690172 03
| Epoch (UTC): | 25 May 2026 10:10:02 |
| Eccentricity: | 0.0001220 |
| inclination: | 53.1580° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 194.1479° |
| argument of perigee: | 90.1537° |
| revolutions per day: | 15.31690172 |
| mean anomaly at epoch: | 269.9604° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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