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 25724U 99023A 25083.14921558 -.00000013 00000-0 -75697-3 0 9999
2 25724 28.2434 340.0521 2131360 257.8574 77.6681 9.37504505 30112
| Epoch (UTC): | 24 March 2025 03:34:52 |
| Eccentricity: | 0.2131360 |
| inclination: | 28.2434° |
| perigee height: | 1097 km |
| apogee height: | 5147 km |
| right ascension of ascending node: | 340.0521° |
| argument of perigee: | 257.8574° |
| revolutions per day: | 9.37504505 |
| mean anomaly at epoch: | 77.6681° |
| orbit number at epoch: | 3011 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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