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 67164U 26145.54602183 +.00000000 +00000-0 +51003-3 0 00006
2 67164 42.9989 236.3013 0001262 277.6477 82.4231 15.27591403 03
| Epoch (UTC): | 25 May 2026 13:06:16 |
| Eccentricity: | 0.0001262 |
| inclination: | 42.9989° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 236.3013° |
| argument of perigee: | 277.6477° |
| revolutions per day: | 15.27591403 |
| mean anomaly at epoch: | 82.4231° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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