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 39446U 13066AG 25137.81363682 .00005607 00000-0 53408-3 0 9998
2 39446 97.8229 88.8695 0052828 192.6752 167.3143 14.92731483618514
| Epoch (UTC): | 17 May 2025 19:31:38 |
| Eccentricity: | 0.0052828 |
| inclination: | 97.8229° |
| perigee height: | 552 km |
| apogee height: | 626 km |
| right ascension of ascending node: | 88.8695° |
| argument of perigee: | 192.6752° |
| revolutions per day: | 14.92731483 |
| mean anomaly at epoch: | 167.3143° |
| orbit number at epoch: | 61851 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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