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 00876U 64053A 23157.51351576 .00000115 00000-0 41778-4 0 9998
2 00876 65.0608 352.1623 0145768 330.3118 28.9766 14.64218636126558
| Epoch (UTC): | 06 June 2023 12:19:27 |
| Eccentricity: | 0.0145768 |
| inclination: | 65.0608° |
| perigee height: | 577 km |
| apogee height: | 782 km |
| right ascension of ascending node: | 352.1623° |
| argument of perigee: | 330.3118° |
| revolutions per day: | 14.64218636 |
| mean anomaly at epoch: | 28.9766° |
| orbit number at epoch: | 12655 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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