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 39026U 12072A 23030.45262673 .00033230 00000-0 65035-3 0 9998
2 39026 97.2816 25.1114 0026696 63.8610 296.5382 15.46949287563871
| Epoch (UTC): | 30 January 2023 10:51:46 |
| Eccentricity: | 0.0026696 |
| inclination: | 97.2816° |
| perigee height: | 407 km |
| apogee height: | 444 km |
| right ascension of ascending node: | 25.1114° |
| argument of perigee: | 63.8610° |
| revolutions per day: | 15.46949287 |
| mean anomaly at epoch: | 296.5382° |
| orbit number at epoch: | 56387 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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