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 61528U 26145.40743544 +.00000000 +00000-0 +37487-4 0 00007
2 61528 53.1593 146.4175 0001165 77.8797 282.2334 15.30196565 01
| Epoch (UTC): | 25 May 2026 09:46:42 |
| Eccentricity: | 0.0001165 |
| inclination: | 53.1593° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 146.4175° |
| argument of perigee: | 77.8797° |
| revolutions per day: | 15.30196565 |
| mean anomaly at epoch: | 282.2334° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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