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 25168.03686885 .00000536 00000-0 30768-3 0 9995
2 12 32.9047 71.5145 1648944 332.2122 19.9105 11.47756074731923
| Epoch (UTC): | 17 June 2025 00:53:05 |
| Eccentricity: | 0.1648944 |
| inclination: | 32.9047° |
| perigee height: | 554 km |
| apogee height: | 3292 km |
| right ascension of ascending node: | 71.5145° |
| argument of perigee: | 332.2122° |
| revolutions per day: | 11.47756074 |
| mean anomaly at epoch: | 19.9105° |
| orbit number at epoch: | 73192 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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