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 67146U 26145.16223213 +.00000000 +00000-0 +41608-3 0 00007
2 67146 51.8993 94.9395 0000837 75.3536 284.7519 14.79942268 05
| Epoch (UTC): | 25 May 2026 03:53:36 |
| Eccentricity: | 0.0000837 |
| inclination: | 51.8993° |
| perigee height: | 629 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 94.9395° |
| argument of perigee: | 75.3536° |
| revolutions per day: | 14.79942268 |
| mean anomaly at epoch: | 284.7519° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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