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 33493U 09002B 25105.87867026 .11018114 29792-5 14588-2 0 9999
2 33493 98.1265 195.2801 0014877 274.5743 85.3852 16.35215587885656
| Epoch (UTC): | 15 April 2025 21:05:17 |
| Eccentricity: | 0.0014877 |
| inclination: | 98.1265° |
| perigee height: | 169 km |
| apogee height: | 188 km |
| right ascension of ascending node: | 195.2801° |
| argument of perigee: | 274.5743° |
| revolutions per day: | 16.35215587 |
| mean anomaly at epoch: | 85.3852° |
| orbit number at epoch: | 88565 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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