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 67381U 26144.95278601 +.00000000 +00000-0 +73380-4 0 00008
2 67381 97.8040 144.0234 0005001 181.4491 178.6712 14.88239933 09
| Epoch (UTC): | 24 May 2026 22:52:00 |
| Eccentricity: | 0.0005001 |
| inclination: | 97.8040° |
| perigee height: | 600 km |
| apogee height: | 607 km |
| right ascension of ascending node: | 144.0234° |
| argument of perigee: | 181.4491° |
| revolutions per day: | 14.88239933 |
| mean anomaly at epoch: | 178.6712° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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