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 09482U 76102B 25187.97796913 .00000101 00000-0 50229-4 0 9997
2 09482 81.2548 144.3058 0085636 139.3084 221.4527 14.07910024501449
| Epoch (UTC): | 06 July 2025 23:28:16 |
| Eccentricity: | 0.0085636 |
| inclination: | 81.2548° |
| perigee height: | 804 km |
| apogee height: | 928 km |
| right ascension of ascending node: | 144.3058° |
| argument of perigee: | 139.3084° |
| revolutions per day: | 14.07910024 |
| mean anomaly at epoch: | 221.4527° |
| orbit number at epoch: | 50144 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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