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 48375U 26145.00104281 +.00000000 +00000-0 +25201-3 0 00007
2 48375 53.1595 352.8812 0001109 88.7619 271.3510 15.31715889 03
| Epoch (UTC): | 25 May 2026 00:01:30 |
| Eccentricity: | 0.0001109 |
| inclination: | 53.1595° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 352.8812° |
| argument of perigee: | 88.7619° |
| revolutions per day: | 15.31715889 |
| mean anomaly at epoch: | 271.3510° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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