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 25107.84689691 .00008399 00000-0 80498-3 0 9999
2 39446 97.8200 59.0977 0052134 295.0954 64.4860 14.92365539614040
| Epoch (UTC): | 17 April 2025 20:19:31 |
| Eccentricity: | 0.0052134 |
| inclination: | 97.8200° |
| perigee height: | 554 km |
| apogee height: | 627 km |
| right ascension of ascending node: | 59.0977° |
| argument of perigee: | 295.0954° |
| revolutions per day: | 14.92365539 |
| mean anomaly at epoch: | 64.4860° |
| orbit number at epoch: | 61404 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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