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 67328U 26145.56353332 +.00000000 +00000-0 +56303-3 0 00007
2 67328 43.0006 251.3090 0001383 288.0657 72.0044 15.27591982 08
| Epoch (UTC): | 25 May 2026 13:31:29 |
| Eccentricity: | 0.0001383 |
| inclination: | 43.0006° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 251.3090° |
| argument of perigee: | 288.0657° |
| revolutions per day: | 15.27591982 |
| mean anomaly at epoch: | 72.0044° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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