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 11U 59001A 25198.17090856 .00000666 00000-0 33656-3 0 9992
2 11 32.8746 272.5789 1449084 311.1102 37.2917 11.89928054837287
| Epoch (UTC): | 17 July 2025 04:06:06 |
| Eccentricity: | 0.1449084 |
| inclination: | 32.8746° |
| perigee height: | 552 km |
| apogee height: | 2900 km |
| right ascension of ascending node: | 272.5789° |
| argument of perigee: | 311.1102° |
| revolutions per day: | 11.89928054 |
| mean anomaly at epoch: | 37.2917° |
| orbit number at epoch: | 83728 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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