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 25789U 26150.51297656 +.00000000 +00000-0 +10969-3 0 00007
2 25789 98.2717 31.3670 0094839 337.3789 22.3239 14.51716939 07
| Epoch (UTC): | 30 May 2026 12:18:41 |
| Eccentricity: | 0.0094839 |
| inclination: | 98.2717° |
| perigee height: | 653 km |
| apogee height: | 787 km |
| right ascension of ascending node: | 31.3670° |
| argument of perigee: | 337.3789° |
| revolutions per day: | 14.51716939 |
| mean anomaly at epoch: | 22.3239° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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