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 29U 60002B 25168.44163049 .00000627 00000-0 11493-3 0 9998
2 29 48.3794 317.0896 0022141 139.3691 220.8879 14.78024570488277
| Epoch (UTC): | 17 June 2025 10:35:56 |
| Eccentricity: | 0.0022141 |
| inclination: | 48.3794° |
| perigee height: | 620 km |
| apogee height: | 651 km |
| right ascension of ascending node: | 317.0896° |
| argument of perigee: | 139.3691° |
| revolutions per day: | 14.78024570 |
| mean anomaly at epoch: | 220.8879° |
| orbit number at epoch: | 48827 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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