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 39152U 13018C 25342.21588022 .00005245 00000-0 48675-3 0 9996
2 39152 97.8031 69.0114 0012883 23.2219 336.9581 14.94785624682542
| Epoch (UTC): | 08 December 2025 05:10:52 |
| Eccentricity: | 0.0012883 |
| inclination: | 97.8031° |
| perigee height: | 574 km |
| apogee height: | 592 km |
| right ascension of ascending node: | 69.0114° |
| argument of perigee: | 23.2219° |
| revolutions per day: | 14.94785624 |
| mean anomaly at epoch: | 336.9581° |
| orbit number at epoch: | 68254 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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