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 59925U 26145.56685813 +.00000000 +00000-0 -12040-3 0 00004
2 59925 43.0011 254.5225 0001492 250.7332 109.3358 15.27600185 08
| Epoch (UTC): | 25 May 2026 13:36:16 |
| Eccentricity: | 0.0001492 |
| inclination: | 43.0011° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 254.5225° |
| argument of perigee: | 250.7332° |
| revolutions per day: | 15.27600185 |
| mean anomaly at epoch: | 109.3358° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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