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 39444U 13066AE 25080.58131613 .00018892 00000-0 14783-2 0 9996
2 39444 97.7624 42.3648 0039539 298.4039 61.3201 15.00463180611584
| Epoch (UTC): | 21 March 2025 13:57:05 |
| Eccentricity: | 0.0039539 |
| inclination: | 97.7624° |
| perigee height: | 538 km |
| apogee height: | 593 km |
| right ascension of ascending node: | 42.3648° |
| argument of perigee: | 298.4039° |
| revolutions per day: | 15.00463180 |
| mean anomaly at epoch: | 61.3201° |
| orbit number at epoch: | 61158 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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