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 23036.90850293 .00000964 00000-0 26348-3 0 9997
2 00045 66.6956 1.5503 0258011 332.7784 25.9980 14.34045470203958
| Epoch (UTC): | 05 February 2023 21:48:14 |
| Eccentricity: | 0.0258011 |
| inclination: | 66.6956° |
| perigee height: | 593 km |
| apogee height: | 963 km |
| right ascension of ascending node: | 1.5503° |
| argument of perigee: | 332.7784° |
| revolutions per day: | 14.34045470 |
| mean anomaly at epoch: | 25.9980° |
| orbit number at epoch: | 20395 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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