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 15772U 26076.08107171 +.00000000 +00000-0 +41930-4 0 00002
2 15772 71.1065 72.1113 0033009 115.9384 308.2458 14.21984557 01
| Epoch (UTC): | 17 March 2026 01:56:44 |
| Eccentricity: | 0.0033009 |
| inclination: | 71.1065° |
| perigee height: | 795 km |
| apogee height: | 842 km |
| right ascension of ascending node: | 72.1113° |
| argument of perigee: | 115.9384° |
| revolutions per day: | 14.21984557 |
| mean anomaly at epoch: | 308.2458° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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