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 23029.30656089 .00000873 00000-0 24142-3 0 9999
2 00045 66.6948 21.5960 0257389 338.2444 20.7875 14.34029524202866
| Epoch (UTC): | 29 January 2023 07:21:26 |
| Eccentricity: | 0.0257389 |
| inclination: | 66.6948° |
| perigee height: | 594 km |
| apogee height: | 962 km |
| right ascension of ascending node: | 21.5960° |
| argument of perigee: | 338.2444° |
| revolutions per day: | 14.34029524 |
| mean anomaly at epoch: | 20.7875° |
| orbit number at epoch: | 20286 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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