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 41552U 26145.52805177 +.00000000 +00000-0 +00000-0 0 00003
2 41552 0.0628 44.8020 0003905 0.9370 106.0103 1.00272368 09
| Epoch (UTC): | 25 May 2026 12:40:23 |
| Eccentricity: | 0.0003905 |
| inclination: | 0.0628° |
| perigee height: | 35770 km |
| apogee height: | 35803 km |
| right ascension of ascending node: | 44.8020° |
| argument of perigee: | 0.9370° |
| revolutions per day: | 1.00272368 |
| mean anomaly at epoch: | 106.0103° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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