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 25108.71858142 .00000879 00000-0 14079-3 0 9995
2 33495 98.1547 7.4932 0006711 314.6703 45.3958 14.74269157872090
| Epoch (UTC): | 18 April 2025 17:14:45 |
| Eccentricity: | 0.0006711 |
| inclination: | 98.1547° |
| perigee height: | 643 km |
| apogee height: | 652 km |
| right ascension of ascending node: | 7.4932° |
| argument of perigee: | 314.6703° |
| revolutions per day: | 14.74269157 |
| mean anomaly at epoch: | 45.3958° |
| orbit number at epoch: | 87209 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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