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 00005U 58002B 25106.59002743 .00000233 00000-0 31099-3 0 9997
2 00005 34.2429 191.0238 1840587 15.0525 349.8088 10.85913093396902
| Epoch (UTC): | 16 April 2025 14:09:38 |
| Eccentricity: | 0.1840587 |
| inclination: | 34.2429° |
| perigee height: | 650 km |
| apogee height: | 3821 km |
| right ascension of ascending node: | 191.0238° |
| argument of perigee: | 15.0525° |
| revolutions per day: | 10.85913093 |
| mean anomaly at epoch: | 349.8088° |
| orbit number at epoch: | 39690 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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