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 33496U 09002E 25143.69609500 .00000449 00000-0 75559-4 0 9998
2 33496 98.1710 40.8086 0005999 166.9490 193.1874 14.74433021876582
| Epoch (UTC): | 23 May 2025 16:42:22 |
| Eccentricity: | 0.0005999 |
| inclination: | 98.1710° |
| perigee height: | 643 km |
| apogee height: | 651 km |
| right ascension of ascending node: | 40.8086° |
| argument of perigee: | 166.9490° |
| revolutions per day: | 14.74433021 |
| mean anomaly at epoch: | 193.1874° |
| orbit number at epoch: | 87658 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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