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 44542U 26144.07952799 +.00000000 +00000-0 +00000-0 0 00007
2 44542 54.3948 183.5409 0008197 0.7769 359.2907 1.86229030 04
| Epoch (UTC): | 24 May 2026 01:54:31 |
| Eccentricity: | 0.0008197 |
| inclination: | 54.3948° |
| perigee height: | 21505 km |
| apogee height: | 21551 km |
| right ascension of ascending node: | 183.5409° |
| argument of perigee: | 0.7769° |
| revolutions per day: | 1.86229030 |
| mean anomaly at epoch: | 359.2907° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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