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 15054U 26042.07519892 +.00000000 +00000-0 +19655-2 0 00001
2 15054 51.9722 234.2126 4701403 114.9194 300.4620 6.15303532 04
| Epoch (UTC): | 11 February 2026 01:48:17 |
| Eccentricity: | 0.4701403 |
| inclination: | 51.9722° |
| perigee height: | 287 km |
| apogee height: | 12116 km |
| right ascension of ascending node: | 234.2126° |
| argument of perigee: | 114.9194° |
| revolutions per day: | 6.15303532 |
| mean anomaly at epoch: | 300.4620° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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