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 10967U 78064A 25188.87707054 .00000206 00000-0 96643-4 0 9990
2 10967 108.0095 331.9313 0000860 286.8811 73.2240 14.45860666471128
| Epoch (UTC): | 07 July 2025 21:02:58 |
| Eccentricity: | 0.0000860 |
| inclination: | 108.0095° |
| perigee height: | 738 km |
| apogee height: | 740 km |
| right ascension of ascending node: | 331.9313° |
| argument of perigee: | 286.8811° |
| revolutions per day: | 14.45860666 |
| mean anomaly at epoch: | 73.2240° |
| orbit number at epoch: | 47112 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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