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 52542U 26145.38664850 +.00000000 +00000-0 +26342-4 0 00000
2 52542 53.2120 144.8136 0001068 70.5588 289.5519 15.08839460 01
| Epoch (UTC): | 25 May 2026 09:16:46 |
| Eccentricity: | 0.0001068 |
| inclination: | 53.2120° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 144.8136° |
| argument of perigee: | 70.5588° |
| revolutions per day: | 15.08839460 |
| mean anomaly at epoch: | 289.5519° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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