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 48329U 26145.25735359 +.00000000 +00000-0 +25841-4 0 00000
2 48329 53.1610 104.8597 0001415 99.1183 260.9978 15.31693968 02
| Epoch (UTC): | 25 May 2026 06:10:35 |
| Eccentricity: | 0.0001415 |
| inclination: | 53.1610° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 104.8597° |
| argument of perigee: | 99.1183° |
| revolutions per day: | 15.31693968 |
| mean anomaly at epoch: | 260.9978° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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