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 41918U 17003B 25163.17012014 .00000199 00000-0 64013-4 0 9994
2 41918 86.3974 242.9989 0002821 100.1453 260.0061 14.34218109440200
| Epoch (UTC): | 12 June 2025 04:04:58 |
| Eccentricity: | 0.0002821 |
| inclination: | 86.3974° |
| perigee height: | 775 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 242.9989° |
| argument of perigee: | 100.1453° |
| revolutions per day: | 14.34218109 |
| mean anomaly at epoch: | 260.0061° |
| orbit number at epoch: | 44020 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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