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 48306U 26145.29836328 +.00000000 +00000-0 -18991-6 0 00008
2 48306 53.1595 102.7116 0001285 99.4862 260.6285 15.31702283 04
| Epoch (UTC): | 25 May 2026 07:09:38 |
| Eccentricity: | 0.0001285 |
| inclination: | 53.1595° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 102.7116° |
| argument of perigee: | 99.4862° |
| revolutions per day: | 15.31702283 |
| mean anomaly at epoch: | 260.6285° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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