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 65200U 26145.29139277 +.00000000 +00000-0 +85362-3 0 00001
2 65200 53.1587 156.5637 0001230 83.5473 276.5670 15.34410420 00
| Epoch (UTC): | 25 May 2026 06:59:36 |
| Eccentricity: | 0.0001230 |
| inclination: | 53.1587° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 156.5637° |
| argument of perigee: | 83.5473° |
| revolutions per day: | 15.34410420 |
| mean anomaly at epoch: | 276.5670° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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