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 26065.47639650 +.00000000 +00000-0 +30164-4 0 00003
2 15755 71.1114 132.7384 0033847 147.2109 213.1128 14.20989962 05
| Epoch (UTC): | 06 March 2026 11:26:00 |
| Eccentricity: | 0.0033847 |
| inclination: | 71.1114° |
| perigee height: | 798 km |
| apogee height: | 846 km |
| right ascension of ascending node: | 132.7384° |
| argument of perigee: | 147.2109° |
| revolutions per day: | 14.20989962 |
| mean anomaly at epoch: | 213.1128° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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