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 00694U 63047A 23155.97264844 .00001070 00000-0 12179-3 0 9990
2 00694 30.3600 43.7294 0575192 236.4869 117.9492 14.05263474989273
| Epoch (UTC): | 04 June 2023 23:20:36 |
| Eccentricity: | 0.0575192 |
| inclination: | 30.3600° |
| perigee height: | 458 km |
| apogee height: | 1293 km |
| right ascension of ascending node: | 43.7294° |
| argument of perigee: | 236.4869° |
| revolutions per day: | 14.05263474 |
| mean anomaly at epoch: | 117.9492° |
| orbit number at epoch: | 98927 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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