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 25134.39490897 .00003576 00000-0 34319-3 0 9990
2 39446 97.8226 85.4719 0052621 204.3154 155.5582 14.92701243618000
| Epoch (UTC): | 14 May 2025 09:28:40 |
| Eccentricity: | 0.0052621 |
| inclination: | 97.8226° |
| perigee height: | 553 km |
| apogee height: | 626 km |
| right ascension of ascending node: | 85.4719° |
| argument of perigee: | 204.3154° |
| revolutions per day: | 14.92701243 |
| mean anomaly at epoch: | 155.5582° |
| orbit number at epoch: | 61800 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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