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 21610U 91050F 25198.16138770 .00000216 00000-0 77601-4 0 9997
2 21610 98.2376 253.7672 0004371 76.3214 283.8463 14.42655359785038
| Epoch (UTC): | 17 July 2025 03:52:23 |
| Eccentricity: | 0.0004371 |
| inclination: | 98.2376° |
| perigee height: | 746 km |
| apogee height: | 753 km |
| right ascension of ascending node: | 253.7672° |
| argument of perigee: | 76.3214° |
| revolutions per day: | 14.42655359 |
| mean anomaly at epoch: | 283.8463° |
| orbit number at epoch: | 78503 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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