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 03137U 68012B 25342.79313722 .00000122 00000-0 17422-3 0 9995
2 03137 90.0290 272.9853 0073157 261.5808 97.7046 13.50302395843093
| Epoch (UTC): | 08 December 2025 19:02:07 |
| Eccentricity: | 0.0073157 |
| inclination: | 90.0290° |
| perigee height: | 1016 km |
| apogee height: | 1125 km |
| right ascension of ascending node: | 272.9853° |
| argument of perigee: | 261.5808° |
| revolutions per day: | 13.50302395 |
| mean anomaly at epoch: | 97.7046° |
| orbit number at epoch: | 84309 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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