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 33504U 26152.60474362 +.00000000 +00000-0 +25066-3 0 00008
2 33504 82.4289 188.5104 0009969 201.4872 158.5959 15.45376661 00
| Epoch (UTC): | 01 June 2026 14:30:49 |
| Eccentricity: | 0.0009969 |
| inclination: | 82.4289° |
| perigee height: | 423 km |
| apogee height: | 437 km |
| right ascension of ascending node: | 188.5104° |
| argument of perigee: | 201.4872° |
| revolutions per day: | 15.45376661 |
| mean anomaly at epoch: | 158.5959° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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