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 53392U 26145.27854943 +.00000000 +00000-0 -38105-4 0 00007
2 53392 53.2125 140.2977 0001028 62.0192 298.0904 15.08848719 06
| Epoch (UTC): | 25 May 2026 06:41:06 |
| Eccentricity: | 0.0001028 |
| inclination: | 53.2125° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 140.2977° |
| argument of perigee: | 62.0192° |
| revolutions per day: | 15.08848719 |
| mean anomaly at epoch: | 298.0904° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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