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 25984U 26150.68504807 +.00000000 +00000-0 +42091-3 0 00002
2 25984 45.0386 242.6735 0005064 238.9729 121.0623 14.39163857 02
| Epoch (UTC): | 30 May 2026 16:26:28 |
| Eccentricity: | 0.0005064 |
| inclination: | 45.0386° |
| perigee height: | 758 km |
| apogee height: | 765 km |
| right ascension of ascending node: | 242.6735° |
| argument of perigee: | 238.9729° |
| revolutions per day: | 14.39163857 |
| mean anomaly at epoch: | 121.0623° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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