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 39430U 13066Q 25138.19087077 .00002029 00000-0 32245-3 0 9995
2 39430 97.6859 358.2280 0131107 264.1136 94.5113 14.67558641612121
| Epoch (UTC): | 18 May 2025 04:34:51 |
| Eccentricity: | 0.0131107 |
| inclination: | 97.6859° |
| perigee height: | 576 km |
| apogee height: | 761 km |
| right ascension of ascending node: | 358.2280° |
| argument of perigee: | 264.1136° |
| revolutions per day: | 14.67558641 |
| mean anomaly at epoch: | 94.5113° |
| orbit number at epoch: | 61212 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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