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 14059U 83042B 25197.90582608 .00000127 00000-0 10881-3 0 9999
2 14059 82.9706 30.4088 0041074 253.9059 105.7576 13.79067868122231
| Epoch (UTC): | 16 July 2025 21:44:23 |
| Eccentricity: | 0.0041074 |
| inclination: | 82.9706° |
| perigee height: | 937 km |
| apogee height: | 997 km |
| right ascension of ascending node: | 30.4088° |
| argument of perigee: | 253.9059° |
| revolutions per day: | 13.79067868 |
| mean anomaly at epoch: | 105.7576° |
| orbit number at epoch: | 12223 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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