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 67857U 26145.46225251 +.00000000 +00000-0 +34565-3 0 00007
2 67857 53.1573 207.3729 0001168 82.0567 278.0566 15.30202777 01
| Epoch (UTC): | 25 May 2026 11:05:38 |
| Eccentricity: | 0.0001168 |
| inclination: | 53.1573° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 207.3729° |
| argument of perigee: | 82.0567° |
| revolutions per day: | 15.30202777 |
| mean anomaly at epoch: | 278.0566° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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