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 27432U 02024C 25132.10279338 .00000076 00000-0 62131-4 0 9992
2 27432 98.9259 181.2344 0050672 157.8763 256.7064 14.14479583186609
| Epoch (UTC): | 12 May 2025 02:28:01 |
| Eccentricity: | 0.0050672 |
| inclination: | 98.9259° |
| perigee height: | 807 km |
| apogee height: | 880 km |
| right ascension of ascending node: | 181.2344° |
| argument of perigee: | 157.8763° |
| revolutions per day: | 14.14479583 |
| mean anomaly at epoch: | 256.7064° |
| orbit number at epoch: | 18660 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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