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 53130U 26145.61271362 +.00000000 +00000-0 +10089-3 0 00002
2 53130 97.3928 155.9192 0001744 89.2615 270.8823 15.24499255 07
| Epoch (UTC): | 25 May 2026 14:42:18 |
| Eccentricity: | 0.0001744 |
| inclination: | 97.3928° |
| perigee height: | 491 km |
| apogee height: | 493 km |
| right ascension of ascending node: | 155.9192° |
| argument of perigee: | 89.2615° |
| revolutions per day: | 15.24499255 |
| mean anomaly at epoch: | 270.8823° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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