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 18010U 26140.52821971 +.00000000 +00000-0 +38696-3 0 00006
2 18010 63.2969 76.4381 0789548 104.0699 264.9337 13.86047537 04
| Epoch (UTC): | 20 May 2026 12:40:38 |
| Eccentricity: | 0.0789548 |
| inclination: | 63.2969° |
| perigee height: | 365 km |
| apogee height: | 1521 km |
| right ascension of ascending node: | 76.4381° |
| argument of perigee: | 104.0699° |
| revolutions per day: | 13.86047537 |
| mean anomaly at epoch: | 264.9337° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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