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 48460U 26145.21858464 +.00000000 +00000-0 +82008-3 0 00002
2 48460 53.0495 115.1124 0007774 42.9559 317.2065 15.73203532 09
| Epoch (UTC): | 25 May 2026 05:14:45 |
| Eccentricity: | 0.0007774 |
| inclination: | 53.0495° |
| perigee height: | 345 km |
| apogee height: | 355 km |
| right ascension of ascending node: | 115.1124° |
| argument of perigee: | 42.9559° |
| revolutions per day: | 15.73203532 |
| mean anomaly at epoch: | 317.2065° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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