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 14096U 83051B 25189.21554852 -.00000169 00000-0 -25442-3 0 9992
2 14096 72.3004 3.3081 1093042 61.6881 309.0025 12.09943802859810
| Epoch (UTC): | 08 July 2025 05:10:23 |
| Eccentricity: | 0.1093042 |
| inclination: | 72.3004° |
| perigee height: | 760 km |
| apogee height: | 2512 km |
| right ascension of ascending node: | 3.3081° |
| argument of perigee: | 61.6881° |
| revolutions per day: | 12.09943802 |
| mean anomaly at epoch: | 309.0025° |
| orbit number at epoch: | 85981 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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