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 48274U 26087.90697538 +.00000000 +00000-0 +17386-3 0 00006
2 48274 41.4668 91.1438 0003972 51.0046 309.1146 15.61593971 00
| Epoch (UTC): | 28 March 2026 21:46:02 |
| Eccentricity: | 0.0003972 |
| inclination: | 41.4668° |
| perigee height: | 380 km |
| apogee height: | 386 km |
| right ascension of ascending node: | 91.1438° |
| argument of perigee: | 51.0046° |
| revolutions per day: | 15.61593971 |
| mean anomaly at epoch: | 309.1146° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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