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 data is extracted from the following two-line orbital elements,
1 36596U 10027A 25132.20720617 .00006155 00000-0 36431-3 0 9994
2 36596 97.7709 136.6169 0008477 45.6449 314.5474 15.11777235814224
| Epoch (UTC): | 12 May 2025 04:58:22 |
| Eccentricity: | 0.0008477 |
| inclination: | 97.7709° |
| perigee height: | 525 km |
| apogee height: | 536 km |
| right ascension of ascending node: | 136.6169° |
| argument of perigee: | 45.6449° |
| revolutions per day: | 15.11777235 |
| mean anomaly at epoch: | 314.5474° |
| orbit number at epoch: | 81422 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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