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 67609U 26145.59202520 +.00000000 +00000-0 +38920-3 0 00009
2 67609 97.2849 210.7747 0000235 145.1247 215.0011 15.33454387 04
| Epoch (UTC): | 25 May 2026 14:12:30 |
| Eccentricity: | 0.0000235 |
| inclination: | 97.2849° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 210.7747° |
| argument of perigee: | 145.1247° |
| revolutions per day: | 15.33454387 |
| mean anomaly at epoch: | 215.0011° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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