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 24276.85617530 .00005040 00000-0 62189-3 0 9993
2 694 30.3538 230.9107 0561327 162.9735 199.0541 14.08649538 57360
| Epoch (UTC): | 02 October 2024 20:32:53 |
| Eccentricity: | 0.0561327 |
| inclination: | 30.3538° |
| perigee height: | 457 km |
| apogee height: | 1270 km |
| right ascension of ascending node: | 230.9107° |
| argument of perigee: | 162.9735° |
| revolutions per day: | 14.08649538 |
| mean anomaly at epoch: | 199.0541° |
| orbit number at epoch: | 5736 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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