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 48316U 26145.25174961 +.00000000 +00000-0 +13198-4 0 00004
2 48316 53.1616 102.8274 0001223 95.5295 264.5846 15.31700279 03
| Epoch (UTC): | 25 May 2026 06:02:31 |
| Eccentricity: | 0.0001223 |
| inclination: | 53.1616° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 102.8274° |
| argument of perigee: | 95.5295° |
| revolutions per day: | 15.31700279 |
| mean anomaly at epoch: | 264.5846° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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