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 53010U 26145.20399669 +.00000000 +00000-0 -42475-4 0 00001
2 53010 53.2132 110.3613 0001356 80.0091 280.1054 15.08835343 05
| Epoch (UTC): | 25 May 2026 04:53:45 |
| Eccentricity: | 0.0001356 |
| inclination: | 53.2132° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 110.3613° |
| argument of perigee: | 80.0091° |
| revolutions per day: | 15.08835343 |
| mean anomaly at epoch: | 280.1054° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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