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 15360U 84109B 25197.50310174 .00000135 00000-0 11971-3 0 9993
2 15360 82.9394 15.0983 0042660 77.2528 283.3392 13.77016861 47693
| Epoch (UTC): | 16 July 2025 12:04:27 |
| Eccentricity: | 0.0042660 |
| inclination: | 82.9394° |
| perigee height: | 943 km |
| apogee height: | 1006 km |
| right ascension of ascending node: | 15.0983° |
| argument of perigee: | 77.2528° |
| revolutions per day: | 13.77016861 |
| mean anomaly at epoch: | 283.3392° |
| orbit number at epoch: | 4769 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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