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 26072.90275753 +.00000000 +00000-0 +83997-3 0 00007
2 18010 63.2951 265.5038 0796532 102.8230 266.2952 13.84868360 04
| Epoch (UTC): | 13 March 2026 21:39:58 |
| Eccentricity: | 0.0796532 |
| inclination: | 63.2951° |
| perigee height: | 363 km |
| apogee height: | 1530 km |
| right ascension of ascending node: | 265.5038° |
| argument of perigee: | 102.8230° |
| revolutions per day: | 13.84868360 |
| mean anomaly at epoch: | 266.2952° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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