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 65371U 26145.35689242 +.00000000 +00000-0 +28681-3 0 00000
2 65371 53.1577 172.0401 0000942 86.5805 273.5303 15.30201939 00
| Epoch (UTC): | 25 May 2026 08:33:55 |
| Eccentricity: | 0.0000942 |
| inclination: | 53.1577° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 172.0401° |
| argument of perigee: | 86.5805° |
| revolutions per day: | 15.30201939 |
| mean anomaly at epoch: | 273.5303° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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