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 82U 61004B 25174.49038685 .00000200 00000-0 18907-3 0 9993
2 82 38.8621 251.9364 1168129 289.8259 58.0343 12.27659608 32724
| Epoch (UTC): | 23 June 2025 11:46:09 |
| Eccentricity: | 0.1168129 |
| inclination: | 38.8621° |
| perigee height: | 632 km |
| apogee height: | 2486 km |
| right ascension of ascending node: | 251.9364° |
| argument of perigee: | 289.8259° |
| revolutions per day: | 12.27659608 |
| mean anomaly at epoch: | 58.0343° |
| orbit number at epoch: | 3272 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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