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 26071.96403574 +.00000000 +00000-0 +79872-3 0 00003
2 18010 63.2953 268.1252 0796663 102.8067 266.3134 13.84841906 06
| Epoch (UTC): | 12 March 2026 23:08:12 |
| Eccentricity: | 0.0796663 |
| inclination: | 63.2953° |
| perigee height: | 363 km |
| apogee height: | 1530 km |
| right ascension of ascending node: | 268.1252° |
| argument of perigee: | 102.8067° |
| revolutions per day: | 13.84841906 |
| mean anomaly at epoch: | 266.3134° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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