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 61552U 26145.57607463 +.00000000 +00000-0 +16777-3 0 00009
2 61552 88.9851 59.1546 0008436 124.8267 235.3715 14.14457683 00
| Epoch (UTC): | 25 May 2026 13:49:32 |
| Eccentricity: | 0.0008436 |
| inclination: | 88.9851° |
| perigee height: | 838 km |
| apogee height: | 850 km |
| right ascension of ascending node: | 59.1546° |
| argument of perigee: | 124.8267° |
| revolutions per day: | 14.14457683 |
| mean anomaly at epoch: | 235.3715° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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