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 05707U 71114B 25140.45726338 .00000165 00000-0 60444-4 0 9997
2 05707 74.0246 143.3745 0025111 227.2700 132.6341 14.40234887798927
| Epoch (UTC): | 20 May 2025 10:58:27 |
| Eccentricity: | 0.0025111 |
| inclination: | 74.0246° |
| perigee height: | 740 km |
| apogee height: | 775 km |
| right ascension of ascending node: | 143.3745° |
| argument of perigee: | 227.2700° |
| revolutions per day: | 14.40234887 |
| mean anomaly at epoch: | 132.6341° |
| orbit number at epoch: | 79892 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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