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 14277U 26067.02757501 +.00000000 +00000-0 +15846-2 0 00008
2 14277 51.9265 76.9669 5399839 104.7548 318.6213 4.93614243 09
| Epoch (UTC): | 08 March 2026 00:39:42 |
| Eccentricity: | 0.5399839 |
| inclination: | 51.9265° |
| perigee height: | 325 km |
| apogee height: | 16060 km |
| right ascension of ascending node: | 76.9669° |
| argument of perigee: | 104.7548° |
| revolutions per day: | 4.93614243 |
| mean anomaly at epoch: | 318.6213° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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