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 25073.19837915 .00308466 00000-0 30064-2 0 9995
2 33493 98.1531 156.5052 0003535 315.6025 44.4948 15.65244972880478
| Epoch (UTC): | 14 March 2025 04:45:39 |
| Eccentricity: | 0.0003535 |
| inclination: | 98.1531° |
| perigee height: | 370 km |
| apogee height: | 375 km |
| right ascension of ascending node: | 156.5052° |
| argument of perigee: | 315.6025° |
| revolutions per day: | 15.65244972 |
| mean anomaly at epoch: | 44.4948° |
| orbit number at epoch: | 88047 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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