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 is defined by the following mean orbital elements,
1 67852U 26145.44231957 +.00000000 +00000-0 +38401-3 0 00003
2 67852 53.1593 207.9953 0000942 78.9473 281.1634 15.30201032 06
| Epoch (UTC): | 25 May 2026 10:36:56 |
| Eccentricity: | 0.0000942 |
| inclination: | 53.1593° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 207.9953° |
| argument of perigee: | 78.9473° |
| revolutions per day: | 15.30201032 |
| mean anomaly at epoch: | 281.1634° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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