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 45602U 26145.57117564 +.00000000 +00000-0 +11441-3 0 00008
2 45602 97.4869 138.4231 0007384 286.3289 73.7129 15.11696890 09
| Epoch (UTC): | 25 May 2026 13:42:29 |
| Eccentricity: | 0.0007384 |
| inclination: | 97.4869° |
| perigee height: | 526 km |
| apogee height: | 536 km |
| right ascension of ascending node: | 138.4231° |
| argument of perigee: | 286.3289° |
| revolutions per day: | 15.11696890 |
| mean anomaly at epoch: | 73.7129° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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