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 694U 63047A 23274.86994718 .00003769 00000-0 46954-3 0 9995
2 694 30.3560 106.0669 0572221 193.5911 164.8671 14.05954236 5630
| Epoch (UTC): | 01 October 2023 20:52:43 |
| Eccentricity: | 0.0572221 |
| inclination: | 30.3560° |
| perigee height: | 458 km |
| apogee height: | 1288 km |
| right ascension of ascending node: | 106.0669° |
| argument of perigee: | 193.5911° |
| revolutions per day: | 14.05954236 |
| mean anomaly at epoch: | 164.8671° |
| orbit number at epoch: | 563 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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