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 21808U 91076D 25198.49429465 .00003417 00000-0 30277-3 0 9997
2 21808 63.3038 328.1400 0891102 68.3384 301.0101 13.55556758 60591
| Epoch (UTC): | 17 July 2025 11:51:47 |
| Eccentricity: | 0.0891102 |
| inclination: | 63.3038° |
| perigee height: | 390 km |
| apogee height: | 1714 km |
| right ascension of ascending node: | 328.1400° |
| argument of perigee: | 68.3384° |
| revolutions per day: | 13.55556758 |
| mean anomaly at epoch: | 301.0101° |
| orbit number at epoch: | 6059 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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