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 25876U 99041E 25198.90390448 .00001959 00000-0 35537-3 0 9993
2 25876 51.7601 158.2984 0506944 15.9902 345.6390 14.10818054329894
| Epoch (UTC): | 17 July 2025 21:41:37 |
| Eccentricity: | 0.0506944 |
| inclination: | 51.7601° |
| perigee height: | 490 km |
| apogee height: | 1223 km |
| right ascension of ascending node: | 158.2984° |
| argument of perigee: | 15.9902° |
| revolutions per day: | 14.10818054 |
| mean anomaly at epoch: | 345.6390° |
| orbit number at epoch: | 32989 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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