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 48595U 26145.01712072 +.00000000 +00000-0 +72749-4 0 00005
2 48595 53.1598 153.9027 0001226 78.9599 281.1540 15.31711290 00
| Epoch (UTC): | 25 May 2026 00:24:39 |
| Eccentricity: | 0.0001226 |
| inclination: | 53.1598° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 153.9027° |
| argument of perigee: | 78.9599° |
| revolutions per day: | 15.31711290 |
| mean anomaly at epoch: | 281.1540° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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