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 21423U 91042B 25163.35688455 .00000374 00000-0 44617-4 0 9999
2 21423 82.4927 113.6486 0018401 52.7120 307.5767 14.81542276834084
| Epoch (UTC): | 12 June 2025 08:33:54 |
| Eccentricity: | 0.0018401 |
| inclination: | 82.4927° |
| perigee height: | 611 km |
| apogee height: | 637 km |
| right ascension of ascending node: | 113.6486° |
| argument of perigee: | 52.7120° |
| revolutions per day: | 14.81542276 |
| mean anomaly at epoch: | 307.5767° |
| orbit number at epoch: | 83408 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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