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 67493U 26145.62390854 +.00000000 +00000-0 +46203-3 0 00005
2 67493 42.9987 240.2992 0001475 268.9819 91.0864 15.27592031 01
| Epoch (UTC): | 25 May 2026 14:58:25 |
| Eccentricity: | 0.0001475 |
| inclination: | 42.9987° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 240.2992° |
| argument of perigee: | 268.9819° |
| revolutions per day: | 15.27592031 |
| mean anomaly at epoch: | 91.0864° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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