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 20U 59007A 25172.19873049 .00000555 00000-0 20979-3 0 9996
2 20 33.3521 125.6200 1643044 279.7272 62.2291 11.60709996442667
| Epoch (UTC): | 21 June 2025 04:46:10 |
| Eccentricity: | 0.1643044 |
| inclination: | 33.3521° |
| perigee height: | 508 km |
| apogee height: | 3215 km |
| right ascension of ascending node: | 125.6200° |
| argument of perigee: | 279.7272° |
| revolutions per day: | 11.60709996 |
| mean anomaly at epoch: | 62.2291° |
| orbit number at epoch: | 44266 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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