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 61553U 26145.60301941 +.00000000 +00000-0 +15535-3 0 00007
2 61553 88.9847 59.6385 0005566 159.3952 200.7458 14.09002082 00
| Epoch (UTC): | 25 May 2026 14:28:20 |
| Eccentricity: | 0.0005566 |
| inclination: | 88.9847° |
| perigee height: | 859 km |
| apogee height: | 867 km |
| right ascension of ascending node: | 59.6385° |
| argument of perigee: | 159.3952° |
| revolutions per day: | 14.09002082 |
| mean anomaly at epoch: | 200.7458° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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