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 65552U 26145.35792814 +.00000000 +00000-0 +18356-3 0 00009
2 65552 49.9856 145.2587 0010654 176.9547 183.1458 14.84084524 03
| Epoch (UTC): | 25 May 2026 08:35:24 |
| Eccentricity: | 0.0010654 |
| inclination: | 49.9856° |
| perigee height: | 609 km |
| apogee height: | 624 km |
| right ascension of ascending node: | 145.2587° |
| argument of perigee: | 176.9547° |
| revolutions per day: | 14.84084524 |
| mean anomaly at epoch: | 183.1458° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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