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 67169U 26145.53974477 +.00000000 +00000-0 +51281-3 0 00006
2 67169 42.9994 237.1186 0000612 283.4152 76.6632 15.27593576 00
| Epoch (UTC): | 25 May 2026 12:57:13 |
| Eccentricity: | 0.0000612 |
| inclination: | 42.9994° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 237.1186° |
| argument of perigee: | 283.4152° |
| revolutions per day: | 15.27593576 |
| mean anomaly at epoch: | 76.6632° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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