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 33053U 26137.84489233 +.00000000 +00000-0 +75474-4 0 00008
2 33053 25.5824 55.1315 0008054 330.3685 29.6396 15.23761117 06
| Epoch (UTC): | 17 May 2026 20:16:38 |
| Eccentricity: | 0.0008054 |
| inclination: | 25.5824° |
| perigee height: | 489 km |
| apogee height: | 500 km |
| right ascension of ascending node: | 55.1315° |
| argument of perigee: | 330.3685° |
| revolutions per day: | 15.23761117 |
| mean anomaly at epoch: | 29.6396° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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