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 23150.16197914 .00000111 00000-0 53585-4 0 9994
2 00045 66.6952 62.8383 0261102 252.2881 104.9564 14.34216689220192
| Epoch (UTC): | 30 May 2023 03:53:14 |
| Eccentricity: | 0.0261102 |
| inclination: | 66.6952° |
| perigee height: | 591 km |
| apogee height: | 964 km |
| right ascension of ascending node: | 62.8383° |
| argument of perigee: | 252.2881° |
| revolutions per day: | 14.34216689 |
| mean anomaly at epoch: | 104.9564° |
| orbit number at epoch: | 22019 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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