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 61689U 26145.05000486 +.00000000 +00000-0 +33383-4 0 00008
2 61689 53.1594 10.0697 0000872 74.2526 285.8588 15.69711614 00
| Epoch (UTC): | 25 May 2026 01:12:00 |
| Eccentricity: | 0.0000872 |
| inclination: | 53.1594° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 10.0697° |
| argument of perigee: | 74.2526° |
| revolutions per day: | 15.69711614 |
| mean anomaly at epoch: | 285.8588° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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