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 07364U 74052B 25199.64980270 .00000113 00000-0 60226-4 0 9995
2 07364 81.2319 167.8460 0050026 123.4893 237.1071 14.06392674616186
| Epoch (UTC): | 18 July 2025 15:35:42 |
| Eccentricity: | 0.0050026 |
| inclination: | 81.2319° |
| perigee height: | 835 km |
| apogee height: | 908 km |
| right ascension of ascending node: | 167.8460° |
| argument of perigee: | 123.4893° |
| revolutions per day: | 14.06392674 |
| mean anomaly at epoch: | 237.1071° |
| orbit number at epoch: | 61618 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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