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 23435U 94084A 25134.24298299 -.00000008 00000-0 00000-0 0 9991
2 23435 14.5221 357.9314 0005425 281.2315 72.6819 0.99081957 28858
| Epoch (UTC): | 14 May 2025 05:49:53 |
| Eccentricity: | 0.0005425 |
| inclination: | 14.5221° |
| perigee height: | 36100 km |
| apogee height: | 36146 km |
| right ascension of ascending node: | 357.9314° |
| argument of perigee: | 281.2315° |
| revolutions per day: | 0.99081957 |
| mean anomaly at epoch: | 72.6819° |
| orbit number at epoch: | 2885 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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