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 33410U 08053C 25191.56795045 .00003343 00000-0 15536-3 0 9992
2 33410 97.8283 243.1004 0094349 359.1894 0.9170 15.16836332912751
| Epoch (UTC): | 10 July 2025 13:37:50 |
| Eccentricity: | 0.0094349 |
| inclination: | 97.8283° |
| perigee height: | 450 km |
| apogee height: | 580 km |
| right ascension of ascending node: | 243.1004° |
| argument of perigee: | 359.1894° |
| revolutions per day: | 15.16836332 |
| mean anomaly at epoch: | 0.9170° |
| orbit number at epoch: | 91275 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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