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 65421U 26145.53677791 +.00000000 +00000-0 +11476-3 0 00006
2 65421 53.1582 235.1358 0000682 64.6543 295.4529 15.31701636 04
| Epoch (UTC): | 25 May 2026 12:52:57 |
| Eccentricity: | 0.0000682 |
| inclination: | 53.1582° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 235.1358° |
| argument of perigee: | 64.6543° |
| revolutions per day: | 15.31701636 |
| mean anomaly at epoch: | 295.4529° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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