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 48382U 26145.56499255 +.00000000 +00000-0 +67031-4 0 00002
2 48382 53.1617 350.2365 0001234 76.0010 284.1129 15.31699481 02
| Epoch (UTC): | 25 May 2026 13:33:35 |
| Eccentricity: | 0.0001234 |
| inclination: | 53.1617° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 350.2365° |
| argument of perigee: | 76.0010° |
| revolutions per day: | 15.31699481 |
| mean anomaly at epoch: | 284.1129° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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