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 48328U 26145.26168163 +.00000000 +00000-0 +19826-4 0 00009
2 48328 53.1605 104.8476 0001286 91.6868 268.4281 15.31697582 00
| Epoch (UTC): | 25 May 2026 06:16:49 |
| Eccentricity: | 0.0001286 |
| inclination: | 53.1605° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 104.8476° |
| argument of perigee: | 91.6868° |
| revolutions per day: | 15.31697582 |
| mean anomaly at epoch: | 268.4281° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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