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 48378U 26145.59731262 +.00000000 +00000-0 +55172-4 0 00000
2 48378 53.1615 350.3163 0001482 99.2151 260.9019 15.31700398 00
| Epoch (UTC): | 25 May 2026 14:20:07 |
| Eccentricity: | 0.0001482 |
| inclination: | 53.1615° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 350.3163° |
| argument of perigee: | 99.2151° |
| revolutions per day: | 15.31700398 |
| mean anomaly at epoch: | 260.9019° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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