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 25861U 99039B 25191.56977693 .00000310 00000-0 46609-4 0 9995
2 25861 98.0347 245.5083 0014064 327.2466 32.7873 14.81308123401014
| Epoch (UTC): | 10 July 2025 13:40:28 |
| Eccentricity: | 0.0014064 |
| inclination: | 98.0347° |
| perigee height: | 615 km |
| apogee height: | 635 km |
| right ascension of ascending node: | 245.5083° |
| argument of perigee: | 327.2466° |
| revolutions per day: | 14.81308123 |
| mean anomaly at epoch: | 32.7873° |
| orbit number at epoch: | 40101 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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