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 23089.77085352 .00000731 00000-0 20428-3 0 9991
2 00045 66.6940 222.1340 0260872 295.1021 62.3214 14.34149704211538
| Epoch (UTC): | 30 March 2023 18:30:01 |
| Eccentricity: | 0.0260872 |
| inclination: | 66.6940° |
| perigee height: | 591 km |
| apogee height: | 964 km |
| right ascension of ascending node: | 222.1340° |
| argument of perigee: | 295.1021° |
| revolutions per day: | 14.34149704 |
| mean anomaly at epoch: | 62.3214° |
| orbit number at epoch: | 21153 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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