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 23152.13080450 .00000282 00000-0 98925-4 0 9996
2 05707 74.0290 32.5790 0025460 287.9622 71.8758 14.39293046695403
| Epoch (UTC): | 01 June 2023 03:08:21 |
| Eccentricity: | 0.0025460 |
| inclination: | 74.0290° |
| perigee height: | 742 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 32.5790° |
| argument of perigee: | 287.9622° |
| revolutions per day: | 14.39293046 |
| mean anomaly at epoch: | 71.8758° |
| orbit number at epoch: | 69540 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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