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 39232U 13043A 25153.87856145 0.00015000 00000-0 24435-3 0 00
2 39232 97.9094 217.0633 0523650 263.7704 96.2294 14.69933412 05
| Epoch (UTC): | 02 June 2025 21:05:07 |
| Eccentricity: | 0.0523650 |
| inclination: | 97.9094° |
| perigee height: | 292 km |
| apogee height: | 1030 km |
| right ascension of ascending node: | 217.0633° |
| argument of perigee: | 263.7704° |
| revolutions per day: | 14.69933412 |
| mean anomaly at epoch: | 96.2294° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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