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 02825U 67053B 25198.58548459 .00000015 00000-0 48443-4 0 9994
2 02825 69.9718 71.8451 0009477 254.2759 105.7303 13.97641474 45347
| Epoch (UTC): | 17 July 2025 14:03:05 |
| Eccentricity: | 0.0009477 |
| inclination: | 69.9718° |
| perigee height: | 895 km |
| apogee height: | 909 km |
| right ascension of ascending node: | 71.8451° |
| argument of perigee: | 254.2759° |
| revolutions per day: | 13.97641474 |
| mean anomaly at epoch: | 105.7303° |
| orbit number at epoch: | 4534 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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