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 00670U 63038B 23088.72126432 .00000130 00000-0 20649-3 0 9999
2 00670 90.0110 334.6040 0042009 156.9409 203.3636 13.44429414916224
| Epoch (UTC): | 29 March 2023 17:18:37 |
| Eccentricity: | 0.0042009 |
| inclination: | 90.0110° |
| perigee height: | 1061 km |
| apogee height: | 1124 km |
| right ascension of ascending node: | 334.6040° |
| argument of perigee: | 156.9409° |
| revolutions per day: | 13.44429414 |
| mean anomaly at epoch: | 203.3636° |
| orbit number at epoch: | 91622 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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