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 12U 59001B 25174.13014263 .00000452 00000-0 26667-3 0 9998
2 12 32.9012 50.0689 1648410 4.4436 356.8987 11.47761357732623
| Epoch (UTC): | 23 June 2025 03:07:24 |
| Eccentricity: | 0.1648410 |
| inclination: | 32.9012° |
| perigee height: | 555 km |
| apogee height: | 3292 km |
| right ascension of ascending node: | 50.0689° |
| argument of perigee: | 4.4436° |
| revolutions per day: | 11.47761357 |
| mean anomaly at epoch: | 356.8987° |
| orbit number at epoch: | 73262 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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