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 15755U 26073.57181703 +.00000000 +00000-0 +69560-4 0 00006
2 15755 71.1102 115.6660 0033410 134.0217 226.3671 14.20990972 01
| Epoch (UTC): | 14 March 2026 13:43:24 |
| Eccentricity: | 0.0033410 |
| inclination: | 71.1102° |
| perigee height: | 798 km |
| apogee height: | 846 km |
| right ascension of ascending node: | 115.6660° |
| argument of perigee: | 134.0217° |
| revolutions per day: | 14.20990972 |
| mean anomaly at epoch: | 226.3671° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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