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 00045U 60007A 23332.36631123 .00000446 00000-0 13867-3 0 9992
2 00045 66.6940 302.1806 0246728 119.8470 242.7401 14.34451041246325
| Epoch (UTC): | 28 November 2023 08:47:29 |
| Eccentricity: | 0.0246728 |
| inclination: | 66.6940° |
| perigee height: | 600 km |
| apogee height: | 953 km |
| right ascension of ascending node: | 302.1806° |
| argument of perigee: | 119.8470° |
| revolutions per day: | 14.34451041 |
| mean anomaly at epoch: | 242.7401° |
| orbit number at epoch: | 24632 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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