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 26146.08338808 +.00000000 +00000-0 +59619-3 0 00003
2 18010 63.2975 60.8949 0789115 104.1752 264.8204 13.86138388 06
| Epoch (UTC): | 26 May 2026 02:00:04 |
| Eccentricity: | 0.0789115 |
| inclination: | 63.2975° |
| perigee height: | 365 km |
| apogee height: | 1520 km |
| right ascension of ascending node: | 60.8949° |
| argument of perigee: | 104.1752° |
| revolutions per day: | 13.86138388 |
| mean anomaly at epoch: | 264.8204° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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