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 59378U 26144.74189830 +.00000000 +00000-0 +33219-4 0 00004
2 59378 53.1610 262.5261 0001148 72.4661 287.6465 15.30189118 09
| Epoch (UTC): | 24 May 2026 17:48:20 |
| Eccentricity: | 0.0001148 |
| inclination: | 53.1610° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 262.5261° |
| argument of perigee: | 72.4661° |
| revolutions per day: | 15.30189118 |
| mean anomaly at epoch: | 287.6465° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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