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 65440U 26145.32880331 +.00000000 +00000-0 +32891-3 0 00004
2 65440 97.4486 359.6108 0002688 83.4113 276.7420 15.05660996 00
| Epoch (UTC): | 25 May 2026 07:53:28 |
| Eccentricity: | 0.0002688 |
| inclination: | 97.4486° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 359.6108° |
| argument of perigee: | 83.4113° |
| revolutions per day: | 15.05660996 |
| mean anomaly at epoch: | 276.7420° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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