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 24720U 97005A 25108.85253013 .00000246 00000-0 12562-2 0 9999
2 24720 31.1534 186.8069 5976518 161.6569 233.2438 3.84597289393406
| Epoch (UTC): | 18 April 2025 20:27:38 |
| Eccentricity: | 0.5976518 |
| inclination: | 31.1534° |
| perigee height: | 545 km |
| apogee height: | 21114 km |
| right ascension of ascending node: | 186.8069° |
| argument of perigee: | 161.6569° |
| revolutions per day: | 3.84597289 |
| mean anomaly at epoch: | 233.2438° |
| orbit number at epoch: | 39340 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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