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 39211U 13037D 25197.68115446 .00008428 00000-0 27763-3 0 9999
2 39211 97.9789 90.3897 0079852 18.5167 341.8947 15.28670605659479
| Epoch (UTC): | 16 July 2025 16:20:51 |
| Eccentricity: | 0.0079852 |
| inclination: | 97.9789° |
| perigee height: | 425 km |
| apogee height: | 534 km |
| right ascension of ascending node: | 90.3897° |
| argument of perigee: | 18.5167° |
| revolutions per day: | 15.28670605 |
| mean anomaly at epoch: | 341.8947° |
| orbit number at epoch: | 65947 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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