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 18362U 26053.84576844 +.00000000 +00000-0 +82164-4 0 00000
2 18362 90.3665 82.4041 0106686 42.2023 140.9394 13.44462113 09
| Epoch (UTC): | 22 February 2026 20:17:54 |
| Eccentricity: | 0.0106686 |
| inclination: | 90.3665° |
| perigee height: | 1013 km |
| apogee height: | 1172 km |
| right ascension of ascending node: | 82.4041° |
| argument of perigee: | 42.2023° |
| revolutions per day: | 13.44462113 |
| mean anomaly at epoch: | 140.9394° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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