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 48333U 26145.18278843 +.00000000 +00000-0 +58542-4 0 00001
2 48333 53.1592 105.2618 0001171 85.9913 274.1222 15.31697138 00
| Epoch (UTC): | 25 May 2026 04:23:12 |
| Eccentricity: | 0.0001171 |
| inclination: | 53.1592° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 105.2618° |
| argument of perigee: | 85.9913° |
| revolutions per day: | 15.31697138 |
| mean anomaly at epoch: | 274.1222° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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