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 48312U 26145.26331008 +.00000000 +00000-0 +50283-4 0 00004
2 48312 53.1589 92.2683 0001187 89.1927 270.9210 15.31704250 03
| Epoch (UTC): | 25 May 2026 06:19:09 |
| Eccentricity: | 0.0001187 |
| inclination: | 53.1589° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 92.2683° |
| argument of perigee: | 89.1927° |
| revolutions per day: | 15.31704250 |
| mean anomaly at epoch: | 270.9210° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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