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 25113.05568327 0.00000000 00000-0 00000-0 0 04
2 41334 123.0032 342.3664 0004353 161.6141 198.3859 13.41422777 02
| Epoch (UTC): | 23 April 2025 01:20:11 |
| Eccentricity: | 0.0004353 |
| inclination: | 123.0032° |
| perigee height: | 1101 km |
| apogee height: | 1107 km |
| right ascension of ascending node: | 342.3664° |
| argument of perigee: | 161.6141° |
| revolutions per day: | 13.41422777 |
| mean anomaly at epoch: | 198.3859° |
| 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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