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 45246U 26145.60918612 +.00000000 +00000-0 +00000-0 0 00005
2 45246 0.0132 260.6867 0000685 74.0122 256.0681 1.00271214 05
| Epoch (UTC): | 25 May 2026 14:37:13 |
| Eccentricity: | 0.0000685 |
| inclination: | 0.0132° |
| perigee height: | 35784 km |
| apogee height: | 35790 km |
| right ascension of ascending node: | 260.6867° |
| argument of perigee: | 74.0122° |
| revolutions per day: | 1.00271214 |
| mean anomaly at epoch: | 256.0681° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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