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 25191.52934037 .00000069 00000-0 34327-4 0 9998
2 00876 65.0596 255.0693 0125895 30.0104 330.8135 14.65404470238609
| Epoch (UTC): | 10 July 2025 12:42:15 |
| Eccentricity: | 0.0125895 |
| inclination: | 65.0596° |
| perigee height: | 587 km |
| apogee height: | 764 km |
| right ascension of ascending node: | 255.0693° |
| argument of perigee: | 30.0104° |
| revolutions per day: | 14.65404470 |
| mean anomaly at epoch: | 330.8135° |
| orbit number at epoch: | 23860 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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