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 48399U 26145.26298551 +.00000000 +00000-0 +36919-4 0 00004
2 48399 53.1605 336.4267 0001526 88.1956 271.9220 15.31697848 02
| Epoch (UTC): | 25 May 2026 06:18:41 |
| Eccentricity: | 0.0001526 |
| inclination: | 53.1605° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 336.4267° |
| argument of perigee: | 88.1956° |
| revolutions per day: | 15.31697848 |
| mean anomaly at epoch: | 271.9220° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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