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 41334U 16010A 25325.23096403 0.00000040 00000-0 71609-4 0 01
2 41334 123.0001 280.8302 0005254 143.7147 216.2852 13.41446815 03
| Epoch (UTC): | 21 November 2025 05:32:35 |
| Eccentricity: | 0.0005254 |
| inclination: | 123.0001° |
| perigee height: | 1100 km |
| apogee height: | 1108 km |
| right ascension of ascending node: | 280.8302° |
| argument of perigee: | 143.7147° |
| revolutions per day: | 13.41446815 |
| mean anomaly at epoch: | 216.2852° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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