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 48105U 26145.59730303 +.00000000 +00000-0 -39965-4 0 00006
2 48105 53.1599 103.5455 0001595 97.7248 262.3935 15.31685328 04
| Epoch (UTC): | 25 May 2026 14:20:06 |
| Eccentricity: | 0.0001595 |
| inclination: | 53.1599° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 103.5455° |
| argument of perigee: | 97.7248° |
| revolutions per day: | 15.31685328 |
| mean anomaly at epoch: | 262.3935° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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