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 67417U 26145.44234274 +.00000000 +00000-0 +31669-3 0 00004
2 67417 43.0027 164.6254 0000836 257.0503 103.0255 15.27584761 02
| Epoch (UTC): | 25 May 2026 10:36:58 |
| Eccentricity: | 0.0000836 |
| inclination: | 43.0027° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 164.6254° |
| argument of perigee: | 257.0503° |
| revolutions per day: | 15.27584761 |
| mean anomaly at epoch: | 103.0255° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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