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 65331U 26145.44141647 +.00000000 +00000-0 +62209-3 0 00002
2 65331 53.1602 209.8240 0000705 39.9667 320.1386 15.31704974 08
| Epoch (UTC): | 25 May 2026 10:35:38 |
| Eccentricity: | 0.0000705 |
| inclination: | 53.1602° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 209.8240° |
| argument of perigee: | 39.9667° |
| revolutions per day: | 15.31704974 |
| mean anomaly at epoch: | 320.1386° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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