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 67876U 26145.44337132 +.00000000 +00000-0 +66685-3 0 00006
2 67876 53.1589 207.9684 0001165 84.0195 276.0938 15.30201522 09
| Epoch (UTC): | 25 May 2026 10:38:27 |
| Eccentricity: | 0.0001165 |
| inclination: | 53.1589° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 207.9684° |
| argument of perigee: | 84.0195° |
| revolutions per day: | 15.30201522 |
| mean anomaly at epoch: | 276.0938° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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