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 8344U 75094B 25189.14583284 .00000168 00000-0 61217-4 0 9990
2 8344 74.0561 100.1644 0021835 340.9267 19.1068 14.40419236609116
| Epoch (UTC): | 08 July 2025 03:29:59 |
| Eccentricity: | 0.0021835 |
| inclination: | 74.0561° |
| perigee height: | 741 km |
| apogee height: | 772 km |
| right ascension of ascending node: | 100.1644° |
| argument of perigee: | 340.9267° |
| revolutions per day: | 14.40419236 |
| mean anomaly at epoch: | 19.1068° |
| orbit number at epoch: | 60911 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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