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 00059U 60013B 25339.26538954 .00000113 00000-0 33017-4 0 9991
2 00059 28.2494 39.9639 0188955 127.6748 234.1095 13.53154098216883
| Epoch (UTC): | 05 December 2025 06:22:09 |
| Eccentricity: | 0.0188955 |
| inclination: | 28.2494° |
| perigee height: | 920 km |
| apogee height: | 1201 km |
| right ascension of ascending node: | 39.9639° |
| argument of perigee: | 127.6748° |
| revolutions per day: | 13.53154098 |
| mean anomaly at epoch: | 234.1095° |
| orbit number at epoch: | 21688 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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