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 00029U 60002B 25138.62804399 .00000942 00000-0 15805-3 0 9996
2 00029 48.3777 98.6016 0022492 8.3219 351.8063 14.77970195483754
| Epoch (UTC): | 18 May 2025 15:04:23 |
| Eccentricity: | 0.0022492 |
| inclination: | 48.3777° |
| perigee height: | 620 km |
| apogee height: | 651 km |
| right ascension of ascending node: | 98.6016° |
| argument of perigee: | 8.3219° |
| revolutions per day: | 14.77970195 |
| mean anomaly at epoch: | 351.8063° |
| orbit number at epoch: | 48375 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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