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 67988U 26145.54159809 +.00000000 +00000-0 +63366-3 0 00007
2 67988 42.9989 335.2224 0000939 254.9296 105.1452 15.27600316 09
| Epoch (UTC): | 25 May 2026 12:59:54 |
| Eccentricity: | 0.0000939 |
| inclination: | 42.9989° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 335.2224° |
| argument of perigee: | 254.9296° |
| revolutions per day: | 15.27600316 |
| mean anomaly at epoch: | 105.1452° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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