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 08860U 76047A 25138.82941881 .00000100 00000-0 17205-3 0 9995
2 08860 99.9385 336.3447 0040968 280.4272 90.5077 13.68188464442466
Epoch (UTC): | 18 May 2025 19:54:21 |
Eccentricity: | 0.0040968 |
inclination: | 99.9385° |
perigee height: | 976 km |
apogee height: | 1036 km |
right ascension of ascending node: | 336.3447° |
argument of perigee: | 280.4272° |
revolutions per day: | 13.68188464 |
mean anomaly at epoch: | 90.5077° |
orbit number at epoch: | 44246 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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