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 14700U 84013B 25322.50205235 .00000655 00000-0 73010-4 0 9995
2 14700 82.5347 160.3446 0017370 256.6147 165.5713 14.85449984236067
| Epoch (UTC): | 18 November 2025 12:02:57 |
| Eccentricity: | 0.0017370 |
| inclination: | 82.5347° |
| perigee height: | 600 km |
| apogee height: | 624 km |
| right ascension of ascending node: | 160.3446° |
| argument of perigee: | 256.6147° |
| revolutions per day: | 14.85449984 |
| mean anomaly at epoch: | 165.5713° |
| orbit number at epoch: | 23606 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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