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 67867U 26145.42225977 +.00000000 +00000-0 +39823-3 0 00001
2 67867 53.1590 207.8337 0001245 84.9253 275.1890 15.30213910 09
| Epoch (UTC): | 25 May 2026 10:08:03 |
| Eccentricity: | 0.0001245 |
| inclination: | 53.1590° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 207.8337° |
| argument of perigee: | 84.9253° |
| revolutions per day: | 15.30213910 |
| mean anomaly at epoch: | 275.1890° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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