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 33495U 09002D 25143.67144664 .00000368 00000-0 63439-4 0 9994
2 33495 98.1519 42.6521 0007416 185.1023 175.0111 14.74321913876818
| Epoch (UTC): | 23 May 2025 16:06:52 |
| Eccentricity: | 0.0007416 |
| inclination: | 98.1519° |
| perigee height: | 642 km |
| apogee height: | 652 km |
| right ascension of ascending node: | 42.6521° |
| argument of perigee: | 185.1023° |
| revolutions per day: | 14.74321913 |
| mean anomaly at epoch: | 175.0111° |
| orbit number at epoch: | 87681 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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