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 26073.91366605 +.00000000 +00000-0 +90266-3 0 00003
2 18010 63.2947 262.6802 0796366 102.8411 266.2747 13.84901323 01
| Epoch (UTC): | 14 March 2026 21:55:40 |
| Eccentricity: | 0.0796366 |
| inclination: | 63.2947° |
| perigee height: | 363 km |
| apogee height: | 1530 km |
| right ascension of ascending node: | 262.6802° |
| argument of perigee: | 102.8411° |
| revolutions per day: | 13.84901323 |
| mean anomaly at epoch: | 266.2747° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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