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 39766U 14029A 25189.22612335 .00001176 00000-0 16438-3 0 9996
2 39766 97.9226 286.3268 0001593 98.6233 261.5159 14.79465985600757
| Epoch (UTC): | 08 July 2025 05:25:37 |
| Eccentricity: | 0.0001593 |
| inclination: | 97.9226° |
| perigee height: | 630 km |
| apogee height: | 632 km |
| right ascension of ascending node: | 286.3268° |
| argument of perigee: | 98.6233° |
| revolutions per day: | 14.79465985 |
| mean anomaly at epoch: | 261.5159° |
| orbit number at epoch: | 60075 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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