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 45419U 26145.22705831 +.00000000 +00000-0 +95463-3 0 00002
2 45419 53.0461 140.5960 0008223 3.5514 356.5557 15.64219533 07
| Epoch (UTC): | 25 May 2026 05:26:57 |
| Eccentricity: | 0.0008223 |
| inclination: | 53.0461° |
| perigee height: | 370 km |
| apogee height: | 381 km |
| right ascension of ascending node: | 140.5960° |
| argument of perigee: | 3.5514° |
| revolutions per day: | 15.64219533 |
| mean anomaly at epoch: | 356.5557° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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