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 45230U 26145.32798253 +.00000000 +00000-0 +11274-2 0 00001
2 45230 53.1576 358.6819 0003536 155.4580 204.6595 15.42423806 04
| Epoch (UTC): | 25 May 2026 07:52:17 |
| Eccentricity: | 0.0003536 |
| inclination: | 53.1576° |
| perigee height: | 437 km |
| apogee height: | 441 km |
| right ascension of ascending node: | 358.6819° |
| argument of perigee: | 155.4580° |
| revolutions per day: | 15.42423806 |
| mean anomaly at epoch: | 204.6595° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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