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 67397U 26145.58772527 +.00000000 +00000-0 +26614-3 0 00008
2 67397 97.4540 145.0433 0007414 65.4533 294.7473 15.19275918 09
| Epoch (UTC): | 25 May 2026 14:06:19 |
| Eccentricity: | 0.0007414 |
| inclination: | 97.4540° |
| perigee height: | 503 km |
| apogee height: | 513 km |
| right ascension of ascending node: | 145.0433° |
| argument of perigee: | 65.4533° |
| revolutions per day: | 15.19275918 |
| mean anomaly at epoch: | 294.7473° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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