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 25544U 98067A 25138.86196501 .00008819 00000-0 16460-3 0 9991
2 25544 51.6355 92.3536 0002211 123.9616 236.1583 15.49599819510610
| Epoch (UTC): | 18 May 2025 20:41:13 |
| Eccentricity: | 0.0002211 |
| inclination: | 51.6355° |
| perigee height: | 416 km |
| apogee height: | 419 km |
| right ascension of ascending node: | 92.3536° |
| argument of perigee: | 123.9616° |
| revolutions per day: | 15.49599819 |
| mean anomaly at epoch: | 236.1583° |
| orbit number at epoch: | 51061 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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