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 6966U 73098B 25199.18508996 .00000231 00000-0 74305-4 0 9995
2 6966 74.0552 142.4557 0019529 93.3164 267.0228 14.44607531711575
| Epoch (UTC): | 18 July 2025 04:26:31 |
| Eccentricity: | 0.0019529 |
| inclination: | 74.0552° |
| perigee height: | 729 km |
| apogee height: | 757 km |
| right ascension of ascending node: | 142.4557° |
| argument of perigee: | 93.3164° |
| revolutions per day: | 14.44607531 |
| mean anomaly at epoch: | 267.0228° |
| orbit number at epoch: | 71157 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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