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 57335U 26145.52437431 +.00000000 +00000-0 +16981-4 0 00002
2 57335 43.0022 175.3926 0001118 276.3730 83.6995 15.27575362 01
| Epoch (UTC): | 25 May 2026 12:35:05 |
| Eccentricity: | 0.0001118 |
| inclination: | 43.0022° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 175.3926° |
| argument of perigee: | 276.3730° |
| revolutions per day: | 15.27575362 |
| mean anomaly at epoch: | 83.6995° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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