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 65372U 26145.34423039 +.00000000 +00000-0 +16162-3 0 00001
2 65372 53.1590 171.9541 0001476 76.4467 283.6698 15.30218905 04
| Epoch (UTC): | 25 May 2026 08:15:41 |
| Eccentricity: | 0.0001476 |
| inclination: | 53.1590° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 171.9541° |
| argument of perigee: | 76.4467° |
| revolutions per day: | 15.30218905 |
| mean anomaly at epoch: | 283.6698° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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