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 67384U 26145.44912565 +.00000000 +00000-0 +46457-3 0 00004
2 67384 97.7996 144.2416 0001439 93.6403 266.4977 14.86665691 04
| Epoch (UTC): | 25 May 2026 10:46:44 |
| Eccentricity: | 0.0001439 |
| inclination: | 97.7996° |
| perigee height: | 607 km |
| apogee height: | 609 km |
| right ascension of ascending node: | 144.2416° |
| argument of perigee: | 93.6403° |
| revolutions per day: | 14.86665691 |
| mean anomaly at epoch: | 266.4977° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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