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 25967U 99063A 23080.68207561 -.00000199 00000-0 00000-0 0 9994
2 25967 9.0556 32.4650 0002193 339.7458 29.2973 1.00275252 85481
| Epoch (UTC): | 21 March 2023 16:22:11 |
| Eccentricity: | 0.0002193 |
| inclination: | 9.0556° |
| perigee height: | 35776 km |
| apogee height: | 35794 km |
| right ascension of ascending node: | 32.4650° |
| argument of perigee: | 339.7458° |
| revolutions per day: | 1.00275252 |
| mean anomaly at epoch: | 29.2973° |
| orbit number at epoch: | 8548 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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