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 23336.27079876 .00000877 00000-0 24702-3 0 9995
2 00045 66.6943 291.8793 0246561 116.9549 245.6967 14.34458610246886
| Epoch (UTC): | 02 December 2023 06:29:57 |
| Eccentricity: | 0.0246561 |
| inclination: | 66.6943° |
| perigee height: | 600 km |
| apogee height: | 953 km |
| right ascension of ascending node: | 291.8793° |
| argument of perigee: | 116.9549° |
| revolutions per day: | 14.34458610 |
| mean anomaly at epoch: | 245.6967° |
| orbit number at epoch: | 24688 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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