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 23091.72349847 .00000640 00000-0 18208-3 0 9993
2 00045 66.6942 216.9840 0260939 293.7179 63.6744 14.34152090211813
| Epoch (UTC): | 01 April 2023 17:21:50 |
| Eccentricity: | 0.0260939 |
| inclination: | 66.6942° |
| perigee height: | 591 km |
| apogee height: | 964 km |
| right ascension of ascending node: | 216.9840° |
| argument of perigee: | 293.7179° |
| revolutions per day: | 14.34152090 |
| mean anomaly at epoch: | 63.6744° |
| orbit number at epoch: | 21181 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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