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 61857U 26145.36026698 +.00000000 +00000-0 -76785-4 0 00006
2 61857 43.0010 164.9761 0001277 281.2536 78.8172 15.27593402 06
| Epoch (UTC): | 25 May 2026 08:38:47 |
| Eccentricity: | 0.0001277 |
| inclination: | 43.0010° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 164.9761° |
| argument of perigee: | 281.2536° |
| revolutions per day: | 15.27593402 |
| mean anomaly at epoch: | 78.8172° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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