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 67846U 26145.60285041 +.00000000 +00000-0 +57796-3 0 00005
2 67846 42.9998 192.9698 0002017 261.7279 98.3344 15.27592437 08
| Epoch (UTC): | 25 May 2026 14:28:06 |
| Eccentricity: | 0.0002017 |
| inclination: | 42.9998° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 192.9698° |
| argument of perigee: | 261.7279° |
| revolutions per day: | 15.27592437 |
| mean anomaly at epoch: | 98.3344° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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