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 66636U 26145.43210861 +.00000000 +00000-0 +22156-3 0 00002
2 66636 53.1564 143.6611 0001045 91.9981 268.1139 15.30200655 09
| Epoch (UTC): | 25 May 2026 10:22:14 |
| Eccentricity: | 0.0001045 |
| inclination: | 53.1564° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 143.6611° |
| argument of perigee: | 91.9981° |
| revolutions per day: | 15.30200655 |
| mean anomaly at epoch: | 268.1139° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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